- In this lab, the flow over a Clark Y aerofoil is modelled. The flow is assumed to be twodimensional, viscous and turbulent.
The effect of variation of the angle of attack has
on the lift and drag characteristics of the aerofoil are the main object of this lab as well as the utilizationof different turbulence models when separation occurs for high angles of attack.
Additional details and the geometry will be provided.
8 freelanceria on tarjonnut keskimäärin 52£ tähän työhön
Hello I'm Mohamed Saeed. aerospace engineer with high experience in ANSYS as well well. u can check my profile. I have checked your job description and I'm ready to help you in your project
Hello I'm Navdeep. I have done a lot of similar work and deem myself able to complete your work with best quality and in least [login to view URL] see my sample work, please send me a message. Thanks.
Hi sir, it would my honor to work you in this project. I have a high-performance computer to run the cases of CFD problems so you model will be ready as soon as possible.