Em Andamento

aerodynamics

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.

I want it in One day

Habilidades: Excel, Matlab and Mathematica

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

ID do Projeto: #6805843

5 freelancers estão ofertando em média $20 para este trabalho

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?

$10 USD em 1 dia
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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.

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prodiproy333

Dear Hiring Manager, I’m confident that I will be able to finish the work easily and by time. I have good experience about this job. I have worked on many projects which were very similar to this project. I am Mais

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aquatic7

A proposal has not yet been provided

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