GDyn06set07

# GDyn06set07 - Problem Set 7(PS 7 Due Tuesday March 7 7.1...

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Problem Set 7 (PS 7) Due Tuesday March 7 7.1 Air is flowing in a duct configured like Figure 4.19 in the text with 1 θ =10 degrees, 2 θ = 20 degrees and with Mach Number of 3 in the flow approaching the corner. What is the temperature, pressure and velocity in region 3 after the second reflection ? 7.3 Plot 6 points of a pressure deflection diagram for flows over a wedge with M= 2.6. Include some points for both a weak and strong shock. 7.2 Air is flowing through a duct with corners configured like Figure 4.23 in the text with 1 θ =10 degrees, 2 θ = 20 degrees and with Mach Number of 3 in the flow approaching the corners. What are the temperatures, pressure and velocities in the regions 4 and 4’ ? 7.4. Derive in detail showing all steps equation 4.35 in the test, the governing equation for Prandtl-Meyer flow. In what ways is this equation restricted ?

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() methods D 1 by ate indetermin properties reflect. t won' 30 θ 2.504, M @ β M θ 2.504 θ β /sin M M 1.242 /T T 2.054 /p p
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## This note was uploaded on 07/09/2011 for the course MAE 422 taught by Professor Staff during the Spring '10 term at University of Florida.

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GDyn06set07 - Problem Set 7(PS 7 Due Tuesday March 7 7.1...

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