Unformatted text preview: 80 degrees. Compare to the static pressure ratio for a normal shock in a Mach 2.5. 3. Find the static temperature ratio for an oblique shock in a Mach 1.8 flow and shock angle of 40 degrees. Compare to the static temperature ratio for a Mach 1.8 normal shock. Use normal shock tables to solve these problems: 4. Find the static pressure ratio for an oblique shock in a Mach 2.5 flow with shock angle of 60 degrees. Compare to the static pressure ratio for a normal shock in a Mach 2.5. 5. Find the static temperature ratio across an oblique shock with pressure ratio of 5 and shock angle of 47 degrees. 6. Find the static temperature ratio across a normal shock with pressure ratio of 5....
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This note was uploaded on 02/21/2012 for the course AAE 334 taught by Professor Collicott during the Fall '09 term at Purdue.
 Fall '09
 COLLICOTT

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