aerodynamics -- 2
$10-30 USD
Pago na entrega
I need to find the angle of attack for CL=.40 and also lift coefficient distributions,induced angle of attack distributions and induced drag coefficients for two aspect ratios 6 and 12 for untwisted uncambered rectangular wings.
Also, for the rectangular wing find the same.
ID do Projeto: #6810813
Sobre o projeto
3 freelancers estão ofertando em média $28 nesse trabalho
Hi I am an Electrical Engineer and I have read aerodynamic courses. I have done excellent in Odesk and i am sure that i will best in freelancer..Don't waste your time in hiring other freelancers. Regards Shamail H