f08_ps10_fall03 - Fall 2003 Unified Engineering Fluids...

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Unformatted text preview: Fall 2003 Unified Engineering Fluids Problem F8 F8. A cascade of vanes turns the airflow around each corner of the Wright Brothers Wind Tunnel. Assume the flow parameters are: constant air density: upstream air velocity: vane spacing: vane span: upstream flow angle: downstream flow angle: � = 1.2 kg/m3 V = 30 m/s h = 0.4 m b = 2.5 m 45� −45� Determine the force on each vane. Again, clearly draw a suitable control volume for your analysis. h V ...
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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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