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Unformatted text preview: Mach number. 2. Add the curve through the maximum turning angles as a dashed line. 3. 20% extra credit : add the curve separating subsonic downstream flow from supersonic downstream flow as a solid line. 4. A second useful chart for aerodynamic design, which is not included in your text, is constant Mach number curves showing 1 2 / p p versus turning angle in degrees. Create this chart too. Hand in hard copy of your generously-commented m-file or m-files and hard copies of your appropriately labeled, neat, and legible plots. Also describe how you performed part 3 if you did so. Just list the Mach numbers in the title of the plot, don’t waste time trying to label each curve in the plot (then ponder this: if given an unlabeled oblique shock chart, how could you identify what upstream Mach numbers are plotted?)...
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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