Problem 2 (35%): Consider an airplane with the following characteristics: Weight, W Zero-lift moment coefficient, Go...

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(ituen 22701 N 6 rod 0.34 フ he need t cetentote the anqteatoee at aSso mlsec 2 h (22a 00 0.28 the 9, 35 auseseft degrees. Abs ke le of attack 078

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