aerodynamics -- 2

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.

Habilidades: Excel, Matlab and Mathematica

Veja mais: matlab find, matlab excel, drag excel, aerodynamics aspect aircraft wings 111, blended wing body catia, resize image aspect ratio, flsh wing, chengduchina wing animation, cs2 aspect turn, money aspect web design, image resize aspect ratio, word aspect

Acerca do Empregador:
( 3 comentários ) Denver, United States

ID do Projeto: #6810813

3 freelancers are bidding on average $28 for this job


A proposal has not yet been provided

$35 USD in 4 dias
(15 Comentários)

A proposal has not yet been provided

$15 USD em 1 dia
(0 Comentários)

Dear Client, Greeting of the day ahead !!! Thanks for providing us opportunity to place bid over the project and communicate with you. I am a serious bidder here and i have already worked on a similar project befor Mais

$25 USD em 1 dia
(0 Comentários)

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

$35 USD in 6 dias
(0 Comentários)