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Wind-tunnel tests of the 1/8-scale powered model of the Curtiss XBTC-2 airplane I : preliminary investigation of longitudinal stability
Document ID
19930092677
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wells, Evalyn G
Date Acquired
September 6, 2013
Publication Date
June 1, 1944
Report/Patent Number
NACA-WR-L-667
Report Number: NACA-WR-L-667
Accession Number
93R21967
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ELEVATORS - DEFLECTION
WING SLATS - HANDLEY PAGE
PRESSURE DISTRIBUTION - RADIATORS, OIL
WIND TUNNEL TESTS (NACA-10'X7')(AMER )
STABILITY, LONGITUDINAL - CURTISS BTC-2
WING FLAPS, SKEWED
STALLING CHARACTERISTICS - CURTISS BTC-2
AIRPLANES - CURTISS BTC-2 (EXPERIMENTAL)
TAIL SURFACES, HORIZONTAL - CURTISS BTC-2 WIND TUNNEL TESTS - NACA-10'X7')

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