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 %3D 2.0 m

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 %3D 2.0 m

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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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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