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A system for varying the stability and control of a deflected-jet fixed-wing vtol aircraftVariable control power and augmented stability for hovering VTOL aircraft
Document ID
19650007734
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hegarty, D. M. (NASA Ames Research Center Moffett Field, CA, United States)
Pauli, F. A. (NASA Ames Research Center Moffett Field, CA, United States)
Walsh, T. M. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1965
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-2700
Report Number: NASA-TN-D-2700
Accession Number
65N17335
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HOVERING STABILITY
STABILITY AND CONTROL
VTOL AIRCRAFT
AIRCRAFT CONTROL

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