CHARACTERISTICS OF AIRCRAFT WITH LIFTING-FAN PROPULSION SYSTEMS FOR V/STOL
Wind-tunnel tests on lifting-fan propulsion system for v/stol aircraft - fan-in-fuselage and fan-in-wing configurations are considered
VTOL AIRCRAFT↗
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THE FUTURE OF V/STOL AIRCRAFT
Discussion of the performance of v/stol aircraft and their future in view of some of their general deficiencies
VTOL AIRCRAFT↗
AERODYNAMIC FACTORS TO BE CONSIDERED IN THE DESIGN OF TILT-WING V/STOL AIRPLANES
Aerodynamic considerations in the design of tilt-wing v/stol aircraft
TILT-WING AIRCRAFT↗
JET V/STOL TACTICAL AIRCRAFT
Survey of work done in britain, france and u.s. on jet v/stol aircraft, including the development of lift-engine and vectored-thrust engine designs
STOL AIRCRAFT↗
CHARACTERISTICS OF LIFTING-FAN V/STOL AIRCRAFT
Wind-tunnel tests of full scale practical configuration of lifting fan v/stol aircraft show transition pitching moments comparable to conventional aircraft, and that lift increases with greater forward speed
LIFT FAN↗
The impact of v/stol aircraft on instrument weather operations
Impact of V/STOL aircraft on instrument weather operations
STOL AIRCRAFT↗
Operating problems peculiar to v/stol and stol aircraft
Operating problems of V/STOL and STOL aircraft
VTOL AIRCRAFT↗
Ground effects on v/stol and stol aircraft
Ground effects of V/STOL and STOL aircraft as a result of takeoff
GROUND EFFECT↗
V/stol handling qualities as determined by flight test and simulation techniques.
Bell X-14A test vehicle used to determine control power and damping requirements for V/STOL AIRCRAFT
FLIGHT STABILITY TEST↗
Experimental and theoretical investigation of wind tunnel geometry, emphasizing factors pertinent to V/STOL vehicles testing Progress report no. 1, Sep. 16, 1964 - Mar. 15, 1965
Experimental and theoretical investigation of wind tunnel geometry, emphasizing factors pertinent to V/STOL vehicles testing
VTOL↗
Cruise performance and stability considerations for jet V/STOL aircraft
Cruise performance and aerodynamic stability characteristics of multimission jet V/STOL AIRCRAFT
AERODYNAMIC STABILITY↗
Wind-tunnel investigation of a deflected- slipstream cruise-fan V/STOL aircraft wing
Wind tunnel tests of deflected slipstream cruise fan V/STOL aircraft wing
Newsom, W. A., Jr.↗
Additional studies on the feasibility of V/STOL concepts for short-haul transport aircraft
V/STOL short haul transport design considerations including noise characteristics
Marsh, K. R.↗
Effect of ground proximity on the longitudinal, lateral, and control aerodynamic characteristics of a tilt-wing four-propeller V/STOL model
Ground proximity effects on longitudinal, lateral, and control aerodynamic characteristics of tilt wing four propeller V/STOL wind tunnel model
Goodson, K. W.↗
Technological gaps in V/STOL development
Noise, traffic control, instrument flight, and other problems related to V/STOL aircraft
Kuhn, R. E.↗
Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests
Aerodynamic factors, and effects on dynamic longitudinal stability characteristics of tilt wing V/STOL aircraft
Chambers, J. R.↗
Conjugate gradient methods with an application to V/STOL flight-path optimization
Conjugate gradient methods application to terminal and in-flight constraints for V/STOL flight path optimization
Bryson, A. E., Jr.↗