HW25 - 3. Using the PM_ Matlab functions compute the...

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AAE 334 Fall 2011, Homework 25 Due Wednesday, November 16 at the beginning of class. 1. Compute manually (not using the PM_ Matlab functions) the pressure after a 10 degree expansion corner if the upstream flow is at Mach 2 and pressure of 100 kPa. 2. Compute manually (not using the PM_ Matlab functions) the temperature ratio, 1 2 T T for the flow in the first question.
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Unformatted text preview: 3. Using the PM_ Matlab functions compute the pressure on the upper surface of a flat plate airfoil at Mach 2 in units of upstream pressure. Plot the pressure on the upper surface and the lower surface pressure from HW 24 versus angle of attack. Besides explaining what you did and why, hand in a hard copy of the m-file and your plot....
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