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Unformatted text preview: d. What is the wave angle in degrees for the strong shock solution for an oblique shock at Mach 2.25 and turning angle of 10 degrees? 2. Using the Matlab functions such as OS_tw, OS_mw, OS_mt, or OS_mt_str , and the normal shock functions as needed, compute and plot the static pressure on the bottom of a flat plate airfoil in a Mach 2 flow versus angle of attack for o 10 . Plot in units of 1 p . Hand in hardcopies of your Matlab code and plot....
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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 University-West Lafayette.
- Fall '09