f04_ps09_fall03 - Fall 2003 Unified Engineering Fluids...

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Unformatted text preview: Fall 2003 Unified Engineering Fluids Problem F4 F4. A rectangular wing of chord c and span b is operating in low-speed flow. Its drag depends on the following parameters: D = f (�, �� , V� , µ� , b, c) Determine the dimensionless parameters (Pi products) which determine the drag coefficient CD . ...
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This note was uploaded on 01/28/2012 for the course AERO 16.01 taught by Professor Markdrela during the Fall '05 term at MIT.

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