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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

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Page 1: 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

Page 2: 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

Page 3: 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

Page 4: 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

Page 5: 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

Page 6: 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

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