aerodynamics -- 2

Closed Posted Dec 1, 2014 Paid on delivery

$10-30 USD

Paid on delivery

Closed Paid on delivery

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.

Excel Matlab and Mathematica

Project ID: #6810813

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3 proposals Remote project Active Jan 8, 2015

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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 More

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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

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