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Low-speed investigation of the aerodynamic loads on the droop-nose flap of a wing with leading edge swept back 47.5 degrees and having symmetrical circular-arc airfoil sections at a Reynolds number of 4.3 x 10 (exp 6)
Document ID
19930086026
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Whittle, Edward F , Jr
Fink, Marvin P
Date Acquired
August 16, 2013
Publication Date
January 16, 1950
Report/Patent Number
NACA-RM-L9K04
Report Number: NACA-RM-L9K04
Accession Number
93R15316
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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