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.

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Chapter6: Forced Convection Over Exterior Surfaces
Section: Chapter Questions
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y = 1.4
M = 3.0
8
プ8=20°
%
$ = 40°
X
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 80 = 40°. Calculate the pressure coefficient
at the vertex and estimate the pressure coefficient at point A, where the body angle is 6 =
20° using the method of local cones.
Transcribed Image Text:y = 1.4 M = 3.0 8 プ8=20° % $ = 40° X 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 80 = 40°. Calculate the pressure coefficient at the vertex and estimate the pressure coefficient at point A, where the body angle is 6 = 20° using the method of local cones.
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