aeweb.tamu.eduaeweb.tamu.edu/aero201/tests/Tests_Fall 2009/Exam 3 09...10. Given the wing cross...
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aeweb.tamu.eduaeweb.tamu.edu/aero201/tests/Tests_Fall 2009/Exam 3 09...10. Given the wing cross section affected by wing tip aerodynamics, S on the figure clearly illustrate via vectors