Patran jobs
need FEA expert who familiar with FEA software Patran. have to use Patran..
Complete course author of Nastran - Patran is required. Creation of grouped videos of the main commands and design concepts of each of the main Nastran - Patran modules. Basic practical exercises, medium level and complex step-by-step video tutorials in each module. (10) exercises per modolu approx oriented to the aeronautical or automotive sector Must have the following skills: Expert in Nastran - Patran Good communication skills Proficiency/ Native in english Must be able to make videos (Camtasia or similar programs)
i have a project in that you Need to Model Plate and fastener(By Rutman method) in Patran(must)/nastran. Must use Patran Software. I will provide relevant document and procedure to model the fastener and plate.
We want to compute RMS Von Mises Stress from Nastran Random vibration analysis using the method referred in The following link has a pyhton code (using numpy and pyNastran), which is not working. We want this to work exactly same as MSC Patran random tool to give rms von mises stress.
I need you to develop some software for me. I would like this software to be developed for Windows . MSC Patran Nastran
I would send a PDF, it's something simple.
It´s a simple design in Nastran Patran, simple calculations with beam and shell elements. Must be explained how it was done, it has a little bit of desgin. SOmeone with the right skills could do it in a couple of hours. Thanks
I need you to develop some software for me. I would like this software to be developed for Nastran Patran
In this paper failure analysis of wing-fuselage lug attachment is considered. Aircraft undergoes variable loading condition during its takeoff and landing so maximum lift generated. Wing is subjected to 20% of total load of aircraft and it will cause bending moment and it is high at the root of the wi...material selection, production technique and load spectra may lead to fatigue damage problems are increased significantly. So prediction and analysis of fatigue life is much more important. Maximum tensile stress will cause fatigue crack in that location hence fatigue analysis for variable loading condition using constant S-N amplitude for different stress cycles. CATIA VS5 is used for modeling, MSC/PATRAN used as preprocessor for meshing, MSC/NASTRAN as...
I need to get the non-linear buckling load of a reticulated dome. however I need to include the non-linear properties of the jointing system. I was working in Patran/Nastran , trying to model the connections with non-linear springs being unsuccessful. Please let me know if you are interested. Thanks
I have designed a plate (drawing available on private) and need an AutoCAD drawing together with an FEA analysis such as PATRAN or any other program for the plate (details available upon request).
Are you familiar with Abaqus or Nastran Patran software? I have about 10 number of questions that needs to be solved with any commercial FEM software. I need them to be done in about 5-6 days with amy commercial FEM software. They are fairly easy/moderate type of problem. Let me know if you are able to do this.
Are you familiar with Abaqus or Nastran Patran software? I have about 10 number of questions that needs to be solved with any commercial FEM software. I need them to be done in about 5-6 days with amy commercial FEM software. They are fairly easy/moderate type of problem. Let me know if you are able to do this.
Hi There, Are you familiar with Abaqus or Nastran Patran software? I have about 10 number of questions that needs to be solved with any commercial FEM software. Let me know if you are able to do this, Regards, Yasamin
MSC PATRAN Composite Modelling Must able to incorporate Puck's Failure and Hashin's Failure Able to exhibit elastic-brittle relationship 3D stress, and 2D in plane cases Uniaxial tensile testing Variation of strain rate behavior
Able to perform simulation using Finite Element Modelling using Abaqus/Patran Include failure criteria (library in patran) - pucks, hashins etc plot result and do some simple analysis report writing based on results
Knowledge of MSC Patran Finite Element Modelling 3D First part require modelling of 2/3 phases of objects in contact/interaction Second Part- Composite Modelling with Damage Initiation, Damage Progression in 3D models Plotting the results adn simple analysis Knowledge of composite, fracture mechanics, materials engieneering and mechanical engineering
Hi, Greetings for the d...Composite) of Primary Structures • Airbus Stress Analysis methods • Exposure Fatigue and Damage Tolerant Analysis • Exposures to Airbus tools such as ISAMI, ISSY, and DT tools is an added advantage. • Airbus Stress Analysis methods • Crash and Impact analysis using standard tools • Hand calculation methodologies Desired SKILLS: • Patran/Hypermesh • Nastran analysis • ISAMI, ISSY, and DT tools • NASTRAN • PATRAN • Airbus Stress Analysis methods • Airbus Stress Analysis methods • B. Te...
PLS READ ATTACHED FILES AND PICTURES AND LET ME KNOW IF YOU CAN DO IT ON TIME I DONT HAVE BIG BUDGET FOR THIS PROJECT. LET ME KNOW IF YOU HAVE UNDERSTOOD THIS PROJECT FULLY. MORE INFO: To gain basic knowledge about car body structure. v More extensive reading for gain knowledge about vibration. v To establish reliable and efficienc...establish reliable and efficiency FE model. v Learn basics of structure identification theory. v Understanding non destructive testing on vibration. v Explore various ways of modeling spot welds. v Numerical simulation of welding structure using NASTRAN computer software. I have attached project description and I will email you the the structure that I have to model by using Patran and Nastran computer softwa...
title FE Modelling and Experimental Study of Spot Welds in Car Body Components v To gain basic knowledge about car body structure. v More extensive reading for gain knowledge about vibration. v To establish reliable and efficiency FE model. v Learn basics of structure identification theory. v Understanding non destructive testing on vi...establish reliable and efficiency FE model. v Learn basics of structure identification theory. v Understanding non destructive testing on vibration. v Explore various ways of modeling spot welds. v Numerical simulation of welding structure using NASTRAN computer software. I have attached project description and I will email you the the structure that I have to model by using Patran and Nastran computer...
title FE Modelling and Experimental Study of Spot Welds in Car Body Components v To gain basic knowledge about car body structure. v More extensive reading for gain knowledge about vibration. v To establish reliable and efficiency FE model. v Learn basics of structure identification theory. v Understanding non destructive testing on vi...establish reliable and efficiency FE model. v Learn basics of structure identification theory. v Understanding non destructive testing on vibration. v Explore various ways of modeling spot welds. v Numerical simulation of welding structure using NASTRAN computer software. I have attached project description and I will email you the the structure that I have to model by using Patran and Nastran computer...
title FE Modelling and Experimental Study of Spot Welds in Car Body Components v To gain basic knowledge about car body structure. v More extensive reading for gain knowledge about vibration. v To establish reliable and efficiency FE model. v Learn basics of structure identification theory. v Understanding non destructive testing on vi...establish reliable and efficiency FE model. v Learn basics of structure identification theory. v Understanding non destructive testing on vibration. v Explore various ways of modeling spot welds. v Numerical simulation of welding structure using NASTRAN computer software. I have attached project description and I will email you the the structure that I have to model by using Patran and Nastran computer...
We need an application in PCL (Patran Command Language) that can map the positions of the nodes of a Pam-Stamp results file to a Patran mesh of a similar component in order to perform stress analysis over the deformed component rather than the "perfect" geometry from CAD. Please let us know if you are interested. Thank you in advance.
We need an application in PCL (Patran Command Language) that can map the positions of the nodes of a Pam-Stamp results file to a Patran mesh of a similar component in order to perform stress analysis over the deformed component rather than the "perfect" geometry from CAD. We set the project cost to US$1000 and the time to complete to 15 days but we are open to discuss this. Please let us know if you are interested. Thank you in advance. Aldo Toscano
The goal of the project is to design a working concept of lightweight and strong folding wing. Th...need to be commercially available and reasonably priced. 9. The cost of the mechanism. 10. You can re structure the wing but FEA analysis needs to be provided. You will be given the following items: 1. The CAD model of the wings and its structure. 2. The weight of the wing. 3. The wing and its structure are made of composite material. 4. How we want it to be folded. 5. Wing load data (Patran format or other but discuss with us first). 6. Any other information required can be requested. Milestones: 1. Generate a few and quick concepts. 2. We will choose 1 of the few concepts. 3. You work out the detail from the chosen concept. Please work with Catia V5 or Pro Engine...
Require 4 Stress Engineers - Aerospace who have minimum experience of 7 years using NASTRAN, Patran which are used for Structural Analysis, Fatigue Analysis and Stress Analysis of Aircrafts **** Must Have * We want candidates who are familiar with Airbus and Boeing *** The work location will be Europe for our client who is a Tier 2 vendor After 1 year at the end client's location people will have to work in Bangalore Must be Indians who are already now in Europe on contract jobs Sincerely Ponny Varghese ## Deliverables 1) Complete and fully-functional working program(s) in executable form as well as complete source code of all work done. 2) Deliverables must be in ready-to-run condition, as follows (depending on the nature of the deliverab...
Projeto de Máquina para Lavanderia Industrial Trata-se de uma máquina de Lavanderia industrial já está no mercado há 10 anos, com projeto superdimensionado tanto em sua estrutura metálica, bem como carenagem e fechamentos. Precisamos otimizar este projeto de modo a r...carenagem e fechamentos. Precisamos otimizar este projeto de modo a reduzir no mínimo 20% em matéria prima. Para isso, buscamos um engenheiro mecânico que esteja atuando na área de projetos com análise Estrutural e Dinâmica com experiência de no mínimo 5 anos baseados no Método dos Elementos Finitos – CAE (Computer-Aided Engineerig) utilizando os softwares consagrados como: Ansys, Nastran, Patran, &...
