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Deep-stall aerodynamic characteristics of t-tail aircraftWind tunnel test program for study of aerodynamic characteristics of T-tail aircraft at high angles of attack
Document ID
19650021512
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ray, E. J. (NASA Langley Research Center Hampton, VA, United States)
Taylor, R. T. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Aircraft
Accession Number
65N31113
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
WIND TUNNEL STABILITY TEST
HORIZONTAL TAIL
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