HW32 - sonic. (data and figure below from Airfoil...

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AAE 334, Fall 2011 Homework 32. Due Friday, December 9 at the beginning of class. Solve for critical Mach number as an angle of attack for the following low-speed airfoil pressure data. Use the Prandtl-Glauert rule. List for each case the spanwise position, , where the flow is
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Unformatted text preview: sonic. (data and figure below from Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane, Allison, Dennis O. and Sewall, William G., NASA Langley Research Center, NASA-TP-3516, 1995.)...
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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.

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HW32 - sonic. (data and figure below from Airfoil...

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