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$21 USD / hour
Flag of INDIA
berhampur, india
$21 USD / hour
It's currently 12:22 PM here
Joined July 10, 2020
1 Recommendation

Devbrat N.

@Drexx52

monthly-level-two.svg
5.0 (3 reviews)
2.1
2.1
$21 USD / hour
Flag of INDIA
berhampur, india
$21 USD / hour
100%
Jobs Completed
100%
On Budget
100%
On Time
13%
Repeat Hire Rate

Mechanical-Aerospace Engineer

I am a graduate in Mechanical Engineering and post-graduate diploma in Aerospace Manufacturing. Highly skilled and experience in CAD modelling and CAM tasks using SOLIDWORKS, CATIA, Master-CAM, FUSION 360 and NX. Expertise in CAE (FEA, CFD, Thermal, Vibrations, Shock, etc.) analysis & simulations using ANSYS, ABAQUS, MSC PATRAN, MATLAB and HYPERWORKS. Keen towards Rocket Propulsion and filled with curiosity to learn and implement. Enhanced knowledge on: - Launch Vehicles and Space Systems - Space Mission Engineering - Engineering Design and Optimization - Engineering Materials - Manufacturing & Production (GD&T, Technical Drawing & Process Planning) Core understanding of Mathematics & Physics and versatile to work with fields like: - Robotics - Product Development - Industrial and Space Application projects.
Freelancer Matlab and Mathematica Engineers India

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Portfolio Items

A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A regeneratively cooled Liquid Rocket Engine is designed in two parts: Nozzle and Injector Head/Plate. Both SolidWorks & CATIA are used to complete the CAD model and RPA (Rocket Propulsion Analysis) software is used here for calculating and verifying the engine parameters as well as the oxidizer/fuel mixture ratios and combustion byproducts. 

Further the model is imported to ANSYS workbench for thermal CFD and FEA analyses and combustion simulations.

Engineering Drawing sheets are generated along with the production process planning documents as the model is to be metal 3D printed for prototyping and testing purposes.
Liquid Rocket Engine (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
A 1U CubeSat is designed with standard dimensions and a details computational analysis is performed to verify the structural and design capabilities of the micro satellite.
The CAD model is imported to ANSYS as .STEP file format and the components which were not required for the analysis are suppressed using ANSYS Space claim/ Design modeler. Then the following analyses are performed using ANSYS modules:
1. Quasi-Static Structural Analysis
2. Random Vibration Loading Analysis
3. Harmonic Analysis (Sine Vibration Analysis)
4. Modal Analysis (Natural Frequencies)
5. Response Spectrum Analysis (Shock Vibration Analysis)

All the above analyses are performed and required contours and graphs are drawn and plotted. Materials used in this analysis are AL6061-T6, FR-4 and Stainless Steel.
CUBESAT (Design & Analysis)
CUBESAT (Design & Analysis)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
E-Scooter (Product Design & Development)
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
An E-Scooter is designed using SolidWorks with more than 50 different components that are assembled together and Finite Element Analyses are performed on the model to obtain the maximum stresses and deformation results under loads.
Further Engineering Drawing sheets are generated for each component along with the process planning sheets as the product is under prototyping and few components are manufactured using CNC machines and aerospace grade Aluminum alloys.
E-Scooter (Product Design & Development)
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model.
The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model.
The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model.
The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model.
The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model.
The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model.
The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A radiator plate is in contact with a fluid medium through which hot air is passing. As the solid plate is in contact with hot air, the plate is heating with respect to time. Therefore, a transient thermal analysis is performed on this model.
The model is imported to ANSYS Fluent workbench where the simulation for hot air flow is performed and once the results are obtained for the CFD part, these results are imported to a Transient Thermal Analysis workbench where the results for temperature contours on the solid plate are obtained.
Radiator Plate Thermal Analysis
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
A Can Combustor was designed and imported to ANSYS and Ansys CFX module is used for performing combustion simulations and analysis with various parameters and combustion models to verify which of the results satisfy the required conditions with least amount of emission.
Can Combustor - Combustion Simulation
Complete assembly of knuckle joint mechanism is designed using SolidWorks and Engineering Drawing sheets are generated as well.
Knuckle Joint - Design & Drawing
Complete assembly of knuckle joint mechanism is designed using SolidWorks and Engineering Drawing sheets are generated as well.
Knuckle Joint - Design & Drawing
Knuckle Joint - Design & Drawing
Knuckle Joint - Design & Drawing
Knuckle Joint - Design & Drawing

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5.0
₹1,000.00 INR
In one word I could say he is amazing. I've worked with him on a project regarding aircraft and the way he delivered the project was very professional and perfect. Don't miss a chance to work with him. And also he's not that expensive as other freelancers I've consulted for the project. Even after the project he is ready to help us. Thank you Dev.
CAD/CAM Product Design CATIA Simulation Aircraft Structures
P
Flag of Sai P. @Prashanth659
30 days ago
5.0
$9.70 USD
I wanted to say thanks for guiding me through this task. Devbrat is an absolute joy to work with. He consistently goes above and beyond to achieve the best work for his clients at an affordable price. I could not recommend his service enough and look forward to working with him again in the future.
Matlab and Mathematica Mechanical Engineering Mathematics Aerospace Engineering
+1 more
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Flag of Sabrina D. @SabrinaDesign7
1 month ago
5.0
$50.00 USD
Great work and even gave me more than I needed
Matlab and Mathematica Mechanical Engineering Electrical Engineering Mathematics MATLAB
K
Flag of Howard P. @kilbercolette
2 months ago

Experience

Trainee Engineer

Central Tool Room & Training Centre
Jul 2019 - Jul 2020 (1 year)
- CAD applications: SolidWorks / CATIA / PTC Creo / Fusion 360 / AutoCAD - CAM applications: NX / HyperMILL / MasterCAM - CAE applications: ANSYS / ABAQUS Performing CAD, CAM and CAE tasks for highly quality aerospace manufacturing & production as per aerospace standards AS9100.

Education

Bachelor of Technology (Mechanical Engineering)

Biju Pattnaik University of Technology, India 2015 - 2019
(4 years)

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Matlab and Mathematica 2 Mechanical Engineering 2 Mathematics 2 CAD/CAM 1 Product Design 1

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