aerodynamics -- 2
$10-30 USD
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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.
Nº du projet : #6810813
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3 freelances font une offre moyenne de 28 $ pour ce travail
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