In the figure below, the surface pressure coefficient at point Q on the fuselage of the projectile # 1 is Cp = 0.2. Assuming c/11 = 1/7 and A2 = d1/3, at what Mach number the transonic similarity rule studied in the class could be used to obtain the value of C, at point Q on the fuselage of the projectile # 2? Provide the resulting value of Cp. M, = 1.05 M, =?

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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2. In the figure below, the surface pressure coefficient at point Q on the fuselage of the projectile # 1
is C, = 0.2. Assuming c/a, = 1/7 and A2 = 1/3, at what Mach number the transonic similarity rule
studied in the class could be used to obtain the value of Cp at point Q on the fuselage of the projectile #
2? Provide the resulting value of Cp.
M = 1.05
M, =?
Transcribed Image Text:2. In the figure below, the surface pressure coefficient at point Q on the fuselage of the projectile # 1 is C, = 0.2. Assuming c/a, = 1/7 and A2 = 1/3, at what Mach number the transonic similarity rule studied in the class could be used to obtain the value of Cp at point Q on the fuselage of the projectile # 2? Provide the resulting value of Cp. M = 1.05 M, =?
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