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Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wingFlight simulator study of pitch maneuver speed margins for variable-sweep wing supersonic transport configuration
Document ID
19670028345
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Mc Laughlin, M. D. (NASA Langley Research Center Hampton, VA, United States)
Sawyer, R. H. (NASA Langley Research Center Hampton, VA, United States)
Silsby, N. S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-4170
Report Number: NASA-TN-D-4170
Accession Number
67N37674
Funding Number(s)
CONTRACT_GRANT: 720-05-00-04-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLIGHT SIMULATION
VARIABLE SWEEP
PITCH CONTROL
SUPERSONIC TRANSPORT
AIR SPEED

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