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The unsteady lift of a wing of finite aspect ratioUnsteady-lift functions for wings of finite aspect ratio have been calculated by correcting the aerodynamic inertia and the angle of attack of the infinite wing. The calculations are based on the operational method.
Document ID
19930091758
Document Type
Other
Authors
Jones, Robert T
Date Acquired
September 6, 2013
Publication Date
January 1, 1940
Report/Patent Number
NACA-TR-681
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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