Explore Books on
short take-off and landing aircraft
1-24 of 133 Books
Navy aviation
Navy aviation
By United States. General Accounting Office
Navy aviation
Navy aviation
By United States. General Accounting Office
Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept
Low-speed wind-tunnel test of a STOL supersonic-cruise fighter concept
By Paul L. Coe
Thrust-induced effects on subsonic longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration
Thrust-induced effects on subsonic longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration
By P. Frank Quinto
Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
By Donald R. Riley
A full-scale STOVL ejector experiment
A full-scale STOVL ejector experiment
By Wendy S. Barankiewicz
Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches
Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches
By W. S. Hindson
Powered-lift aircraft technology
Powered-lift aircraft technology
By W. H. Deckert
Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)
Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)
By Jack D. Stephenson
Performance characteristics of a variable-area vane nozzle for vectoring an ASTOVL exhaust jet up to 45
Performance characteristics of a variable-area vane nozzle for vectoring an ASTOVL exhaust jet up to 45
By Jack G. McArdie
The Helio Courier Ultra C/STOL aircraft
By Frank Joseph Rowe
Aerodynamics of V/STOL flight
By Barnes Warnock McCormick
Use of an approximate similarity principle for the thermal scaling of a full-scale thrust augmenting ejector
Use of an approximate similarity principle for the thermal scaling of a full-scale thrust augmenting ejector
By Wendy S. Barankiewicz
Supersonic ejectors
Supersonic ejectors
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
Calculation of the longitudinal aerodynamic characteristics of upper-surface blown wing-flap configurations
Calculation of the longitudinal aerodynamic characteristics of upper-surface blown wing-flap configurations
By M. R. Mendenhall
Status of the Navy's vertical short takeoff and landing aircraft
Status of the Navy's vertical short takeoff and landing aircraft
By United States. General Accounting Office
The lift-fan powered-lift aircraft concept, lessons learned
The lift-fan powered-lift aircraft concept, lessons learned
By W. H. Deckert
Flight evaluation of stabilization and command augumentation system concepts and cockpit displays during approach and landing of a powered-lift STOL aircraft
Flight evaluation of stabilization and command augumentation system concepts and cockpit displays during approach and landing of a powered-lift STOL aircraft
By James A. Franklin
Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches
Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches
By W. S Hindson
Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft
Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft
By Barbara S. Esker