I want to get this project done in 12 hours. it is easy and won't take more than 2 hours.>>
[login to view URL] must investigate the effects of compressibility and shock wave generation over the specific NACA airfoil with Ansys Fluent at various velocities. Subsonic, Transonic,and Supersonic conditions must be [login to view URL] conditions may differ depending on your [login to view URL] of viscous drag will be neglected for ease of calculation (inviscid). Critical Mach Number (by increasing the velocity) and Zero Lift angle(by increasing the attack angle)must be found.
[login to view URL] a NACA 4 Digit generator ([login to view URL] another one you like)
8 freelancers estão ofertando em média $55 nesse trabalho
HELLO DEAR CLIENT I have gone through your project details and the work is DOABLE since its within my area of EXPERTISE.I will tackle are required guideline to deliver desired goal Please consider my bid. THANKS
Hello, I am a professional CAD CAM and CAE design engineer. I am expert in Ansys. I can help you. I hope you contact me as soon possible. Thankyou regards