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Experimental Verification of the Theory of Oscillating AirfoilsMeasurements have been made of the lift on an airfoil in pitching oscillation with a continuous-recording, instantaneous-force balance. The experimental values for the phase difference between the angle of attack and the lift are shown to be in close agreement with theory.
Document ID
19930091748
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Silverstein, Abe
Joyner, Upshur T
Date Acquired
September 6, 2013
Publication Date
January 1, 1939
Report/Patent Number
NACA-TR-673
Report Number: NACA-TR-673
Accession Number
93R21038
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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