Analysing flow over a clark aerofoil using Ansys
£10-20 GBP
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- 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.
项目ID: #18729527
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有6名威客正在参与此工作的竞标,均价£49/小时
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
I am an expert, I have effectively executed numerous designing errands than you can ever envision both on consultant and off consultant. It will be a joy working with you on this one Sir. Much appreciated I HAVE T 更多
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.