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Study of the optimum values of several parameters affecting longitudinal handling qualities of VTOL aircraftOptimum values of pitch rate damping, longitudinal control and speed stability for vertical takeoff aircraft /helicopters/ using pilot ratings
Document ID
19680018681
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Garren, J. F., Jr. (NASA Langley Research Center Hampton, VA, United States)
Kelly, J. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1968
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-4624
Report Number: NASA-TN-D-4624
Accession Number
68N28153
Funding Number(s)
CONTRACT_GRANT: 721-06-00-03-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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