James Hall-Prior
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Create an airfoil in MATLAB
%%%%% part 1 t = .18; tau = .349; e = .0721; a = .574; k = 1.889; c = 2; theta = [0:1:360]; r1 = sqrt(((a*cos(theta)-a)....
2 years 前 | 1 个回答 | 0
Followers: 0 Following: 0
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2 years 前 | 1 个回答 | 0