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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.
- Fall '05