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A simple approximate method for calculating spanwise lift distributions and aerodynamic influence coefficients
Document ID
19930083506
Document Type
Other
Authors
Diederich, Fanklin W
Date Acquired
August 16, 2013
Publication Date
August 1, 1952
Report/Patent Number
NACA-TN-2751
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS, COMPLETE - ASPECT RATIO
WINGS, COMPLETE - SWEEP
LOADS - AEROELASTICITY
WINGS, COMPLETE- TAPER AND TWIST
LOADS, AEODYNAMIC - WINGS

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