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WIND TUNNEL AND LABORATORY TESTS ON THE EDCLIFF 4-15 ANGLE OF PITCH AND YAW TRANSDUCERYaw & pitch angle transducer - wind tunnel & laboratory tests at transonic and supersonic speeds
Document ID
19630012316
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Date Acquired
September 2, 2013
Publication Date
May 14, 1963
Subject Category
Aircraft
Report/Patent Number
MTP-AERO-63-34
NASA-TM-X-50866
Report Number: MTP-AERO-63-34
Report Number: NASA-TM-X-50866
Accession Number
63N22196
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PITCHING MOMENT
TRANSDUCER
YAW

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