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Comparison of control-fixed stability derivatives for two supersonic fighter airplanes as determined from flight and wind-tunnel testsComparison of control-fixed stability derivatives for two supersonic fighters as determined from flight and wind tunnel tests
Document ID
19660022438
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Crane, H. L. (NASA Langley Research Center Hampton, VA, United States)
Mc Laughlin, M. D. (NASA Langley Research Center Hampton, VA, United States)
White, J. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-MEMO-2-3-59L
Report Number: NASA-MEMO-2-3-59L
Accession Number
66N31728
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC AIRCRAFT
CONTROL STABILITY
FLIGHT TEST
WIND TUNNEL

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