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Vibration-Response Tests of a 1/5-Scale Model of the Grumman F6F Airplane in the Langley 16-Foot High-Speed Tunnel
Document ID
19930092477
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Regier, Arthur A
Date Acquired
September 6, 2013
Publication Date
November 1, 1944
Report/Patent Number
NACA-MR-L4K18A
NACA-WR-L-743
Accession Number
93R21767
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS (NACA-HIGH-SPEED-16') (AMER )
AIRPLANES - GRUMMAN F6F
WIND TUNNEL TESTS - NACA - HIGH-SPEED (16')
AIRPLANES - VIBRATION

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