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Langley full-scale-tunnel stability and control tests of the Bell YP-59A airplane
Document ID
19930092470
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Brewer, Gerald W
Date Acquired
September 6, 2013
Publication Date
January 1, 1945
Report/Patent Number
NACA-MR-L5A18
NACA-WR-L-626
Report Number: NACA-MR-L5A18
Report Number: NACA-WR-L-626
Accession Number
93R21760
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRPLANES - BELL P-59A (EXPERIMENTAL)
STABILITY & CONTROL - BELL P-59AS
JET WIND TUNNEL TESTS - NACA FULL-SCALE (AMER )
ENGINES - GENERAL ELECTRIC I-16 (AMER )
TURBOJET

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