Aerodynamics of V/STOL aircraft powered by lift fans
Aerodynamic characteristics of large scale V/STOL powered with lift fans in transition flight
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Aerodynamic characteristics of large scale V/STOL powered with lift fans in transition flight
Aerodynamic characteristics and test data of fan powered V/STOL aircraft
Basic characteristics of propeller, fan, and jet V/STOL aircraft
Wind tunnel model tests of hot gas ingestion and jet interference on jet V/STOL aircraft
Lift, drag, and pitching moments of large V/STOL aircraft models powered by lift fans determined in wind tunnel tests
V/STOL research on controllability, display devices, pilot performance, and terminal guidance
Wind tunnel investigation of hot-gas ingestion and jet interference effects on jet powered V/STOL aircraft
Test sections for small theoretical wind tunnel boundary interference on V/STOL models
Subjective response to far field noise characteristics of V/STOL aircraft sized to carry 60 passengers over 500 mile range
Feasibility of revised V/STOL design and flight plan concepts for short haul transport aircraft
Performance characteristics from static tests in ground effect of V/STOL transport model
Flight control system design data and helicopter simulation data for V/STOL aircraft advanced avionic technology
Exhaust gas reingestion and inlet flow distortion in V/STOL lift engines, discussing static and wind tunnel testing using fighter configuration models
Stopped and stowed rotor V/STOL transport aircraft designs, discussing results of full scale wind tunnel tests of start-stop process
NASA program for developing avionics to provide V/STOL with reliable performance under instrument conditions
Lift engine V/STOL configurations low speed characteristics, measuring exhaust reingestion, inlet pressure, engine and airframe effects in wind tunnels
Progress on experimental program using jet flapped wing model in wind tunnel facilities for testing V/STOL aircraft
Improved method for determining wind tunnel wall effects in V/STOL model testing