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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

Ver 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

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