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A method for predicting the low speed chordwise pressure distribution over sharp edge airfoil sections with plain flaps at the leading and trailing edges
Document ID
19930086336
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Nuber, Robert J
Cahill, Jones F
Date Acquired
August 29, 2013
Publication Date
October 2, 1950
Report/Patent Number
NACA-RM-L50H17a
Report Number: NACA-RM-L50H17a
Accession Number
93R15626
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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