Consider a slender body of revolution at zero angle of attack in supersonic flow with M.. = 3.0 as shown below. The semi-vertex angle is d = 40°. Calculate the pressure coefficient at the vertex and estimate the pressure coefficient at point A, where the body angle is 8 = 20° using the method of local cones.
Consider a slender body of revolution at zero angle of attack in supersonic flow with M.. = 3.0 as shown below. The semi-vertex angle is d = 40°. Calculate the pressure coefficient at the vertex and estimate the pressure coefficient at point A, where the body angle is 8 = 20° using the method of local cones.
Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
8th Edition
ISBN:9781305387102
Author:Kreith, Frank; Manglik, Raj M.
Publisher:Kreith, Frank; Manglik, Raj M.
Chapter6: Forced Convection Over Exterior Surfaces
Section: Chapter Questions
Problem 6.6P
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