What is the main cause of the increase in drag when you increased the angle of attack?

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
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Please solve this question step by step and in clear writing. There is a sub question related to the main question. PLEASE ANSWER THAT AS WELL. Thanks!

What is the main cause of the increase in drag when you increased the
angle of attack?
Transcribed Image Text:What is the main cause of the increase in drag when you increased the angle of attack?
6,4 The leading edge of a supersonic wing is wedge shaped, with a total included angle of 10°.
(See Figure P6.4.) If the wing is flying at zero angle of attack, determine the lift and drag
force on the front portion of the wing per meter of span. Repeat for an angle of attack of 3°.
Assume that the wing is traveling at Mach 2.5.
Leading edge of wing
M, = 2.5
2.0 m
Figure P6.4
Transcribed Image Text:6,4 The leading edge of a supersonic wing is wedge shaped, with a total included angle of 10°. (See Figure P6.4.) If the wing is flying at zero angle of attack, determine the lift and drag force on the front portion of the wing per meter of span. Repeat for an angle of attack of 3°. Assume that the wing is traveling at Mach 2.5. Leading edge of wing M, = 2.5 2.0 m Figure P6.4
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