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Note on the accuracy of a method for rapidly calculating the increments in velocity about an airfoil due to angle of attack
Document ID
19930082562
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Loftin Laurence K , JR
Date Acquired
August 29, 2013
Publication Date
June 1, 1949
Report/Patent Number
NACA-TN-1884
Report Number: NACA-TN-1884
Accession Number
93R11852
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS, SYMMMETRICAL
THEORIES - AIRFOILS - THEODORSEN & GARRICK
AIRFOILS - ANGLE OF ATTACK
FLOW VELOCITY - DISTRIBUTION
FLOW - AIRFOILS
THEORIES - FLOW

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