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Investigation at Supersonic Speeds of Some of the Factors Affecting the Flow over a Rectangular Wing with Symmetrical Circular-arc Section and 30-percent-chord Trailing-edge Flap
Document ID
19930086627
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Czarnecki, K R
Mueller, James N
Date Acquired
August 16, 2013
Publication Date
January 2, 1951
Report/Patent Number
NACA-RM-L50J18
Report Number: NACA-RM-L50J18
Accession Number
93R15917
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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