|SPH modelling with ABAQUS: Tutorial
||Jet of water impinging on the soil. The soil and water should both be modeled as particulate material (particles) with specific properties.
||Matlab and Mathematica, Algorithm, Civil Engineering, Finite Element Analysis, Aerospace Engineering
||Aug 11, 2017
||Aug 11, 20171d 6h
|I would like to hire an Aerospace Engineer
||Program Offline PC Dmis, we have a current and ongoing need for our DCC Global which utilizes PC Dmis software. We are an Aerospace manufacturer and need programs for simple to complex machined parts.
||Aug 8, 2017
||Aug 8, 2017Ended
|Matlab/Simulink Application of a Nonlinear Control Method for a Nonlinear Helicopter Model
||We have nonlinear helicopter model (mainly 8-9 states and 4 inputs) which can be trimmed and linearized around the trim(equilibrium) point. You can offer the control method that you are expert in. We can talk what you need for the design your controller.
||Matlab and Mathematica, Mechanical Engineering, Electrical Engineering, Aeronautical Engineering, Aerospace Engineering
||Jul 21, 2017
||Jul 21, 2017Ended
|Connect joystick with mission planner flight controler
I need help, I am trying to connect joystick with mission planner.
In mission planner, after click on joystick tab, and than click on enable, But mission planner shows that " No joystick- please connect joystick"
Whatever I already connected joystick.
I will send some more details in discussion with image.
The version of mission planner is latest.
Joystick is Logitech extreme 3D.
Flight controler is Pixhawk 2.4.8
Please help to connect joystick with mission planner.
||Research, Aerospace Engineering
||Jul 21, 2017
||Jul 21, 2017Ended
|WINNER GETS 1% OF MACHINE PRODUCTION -- 2
||Each winner will get 1% of the of the machine's production for the rest of the project's duration. Up to 3 winners only. We will sign an agreement.
You basically have to design a giant pressurized Torus with magnets around it's surface in order to propel a 15 ton capsule that loops accelerating inside it at speeds of up to 8 km/sec in a vacuum. Extra thrust can also be given with fuel micro-explosions.
After, the capsule will be redirected (with magnets) to an exit tube that will increase air density on the capsule's way up; with different air layers (separated with paper) in order to reduce the shock-wave and partial destruction of the end of the tube.
Once in the air, the capsule will have a little propulsion system to correct the trajectory, and will be towed by a drone to orbit.
Superconductors and quantum locking might help. We can also disregard the lowest thickest part of the atmosphere by placing the Torus up to 6km high.
||Aerospace Engineering, Mechanical Engineering
||Jul 19, 2017
||Jul 19, 201722d 22h
|Studying, Learning, and Expanding on Fundamental and Complex Aviation Concepts
Currently, I am enrolled in a ground school/instrument rating type class with the hope of soon obtaining my private pilot's license. Though I do have a fabulous instructor, he is a very busy man and is not always available to answer my questions, and/or into go a bit more in depth regarding topics of which I am struggling to develop an adequate understanding.
I know that asking here is a bit of a long shot, but I am looking to find someone who is either a flight instructor or a pilot him/herself, and is willing to take the time to chat with me and to explain/answer questions pertaining to a vast amount of topics in preparation for various FAA tests, and ultimately my check ride!
Thanks so much for any and all help! I really appreciate it!
||Education & Tutoring, Mechanical Engineering, Electrical Engineering, Aeronautical Engineering, Aerospace Engineering
||Jul 14, 2017
||Jul 14, 2017Ended
|Aerodynamic calculations of an electrically powered small uav
||Given a set of airfoils, aircraft geometry and mission profile, you would use calculations to derive aerodynamic coefficients, stability derivatives and performance metrics.
The use of software programs is only accepted to substantiate/confirm calculations.
The delivered coefficients, derivatives and performance metrics are to be in excel format, with formulas used, shown and referenced by (book, page, author).
||Aeronautical Engineering, Aerospace Engineering
||Jul 12, 2017
||Jul 12, 2017Ended
|Project for shazemsaadHazem
||Hi shazemsaadHazem, I noticed your profile and would like to offer you my project. We can discuss any details over chat.
||Matlab and Mathematica, Mechanical Engineering, Civil Engineering, Structural Engineering, , Aerospace Engineering
||Jul 2, 2017
||Jul 2, 2017Ended