aerodynamics

$10-30 USD

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Posted

over 9 years ago

$10-30 USD

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: 6805843

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5 freelancers are bidding on average $20 USD for this job

@Wasif966

Hi. we will be lowest bider Lets Start. 100% job setisfection....Work on very cheap rates...payment after work.. Would you like to discuss more?

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@chaks03

Hi, I could help you with the problem in 12 hours max . Please discuss. Thanks and Regards, Chaks

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@ganesancad

Hello, I have a master degree in aerospace. Please do share complete description of the problem. and Expected results I suppose Prandtl's lifing line theory can be used to solve such a problem.

$30 USD in 1 day