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FLIGHT-DETERMINED STABILITY AND CONTROL DERIVATIVES OF A SUPERSONIC AIRPLANE WITH A LOW-ASPECT-RATIO UNSWEPT WING AND A TEE-TAILFlight-determined stability & control derivatives of supersonic aircraft with low aspect ratio unswept wing & t-tail
Document ID
19630004010
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Andrews, W. H. (NASA Flight Research Center Edwards, CA, United States)
Rediess, H. A. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1959
Subject Category
Biosciences
Report/Patent Number
NASA-MEMO-2-2-59H
Accession Number
63N13886
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY AND CONTROL
LOW ASPECT RATIO WING
T TAIL SURFACE
FLIGHT TEST
UNSWEPT WING
SUPERSONIC AIRCRAFT

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