Add to ORKGThe longitudinal aerodynamic characteristics of a six-fan, tip-driven (remote) lift-fan VTOL transport through transition were determined by an investigation conducted in the Langley V/STOL tunnel. Tests were also made with the large midspan lift-fan pods and lift-cruise fans removed to determine their their influence on the stability and control of the configuration. Data were obtained for a range of model height above ground
Results are presented of a wind-tunnel investigation of the aerodynamic stability, control, and perf...
The purpose of the tests was to obtain overall performance and influencing factors as well as detail...
A low speed wind tunnel test was conducted in the Langley V/STOL tunnel to determine the static long...
A wind-tunnel investigation was conducted in the Langley V/STOL tunnel to determine the longitudinal...
A configuration with outboard pod mounted front fans and rear fans located in the wing trailing-edge...
A wind tunnel test was conducted to obtain power on low speed characteristics of a twin fan vectored...
An investigation was conducted in the NASA-Ames 40 by 80 Foot Wind Tunnel to determine the aerodynam...
Lift, drag, and pitching moments of large V/STOL aircraft models powered by lift fans determined in ...
The low-speed aerodynamic characteristics of large scale V/STOL transport models with lift fan and l...
Aerodynamic characteristics of V/STOL transport model with tandem lift fans mounted at mid-semispan ...
Aerodynamic characteristics of lift fan installation for direct lift V/STOL aircraf
Results are presented of a wind-tunnel investigation of the longitudinal stability, control, and per...
"An investigation of the aerodynamic characteristics of a powered semispan tilting-shrouded-propelle...
A low speed investigation was conducted in the Langley V/STOL tunnel to define the static stability ...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
Results are presented of a wind-tunnel investigation of the aerodynamic stability, control, and perf...
The purpose of the tests was to obtain overall performance and influencing factors as well as detail...
A low speed wind tunnel test was conducted in the Langley V/STOL tunnel to determine the static long...
A wind-tunnel investigation was conducted in the Langley V/STOL tunnel to determine the longitudinal...
A configuration with outboard pod mounted front fans and rear fans located in the wing trailing-edge...
A wind tunnel test was conducted to obtain power on low speed characteristics of a twin fan vectored...
An investigation was conducted in the NASA-Ames 40 by 80 Foot Wind Tunnel to determine the aerodynam...
Lift, drag, and pitching moments of large V/STOL aircraft models powered by lift fans determined in ...
The low-speed aerodynamic characteristics of large scale V/STOL transport models with lift fan and l...
Aerodynamic characteristics of V/STOL transport model with tandem lift fans mounted at mid-semispan ...
Aerodynamic characteristics of lift fan installation for direct lift V/STOL aircraf
Results are presented of a wind-tunnel investigation of the longitudinal stability, control, and per...
"An investigation of the aerodynamic characteristics of a powered semispan tilting-shrouded-propelle...
A low speed investigation was conducted in the Langley V/STOL tunnel to define the static stability ...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
Results are presented of a wind-tunnel investigation of the aerodynamic stability, control, and perf...
The purpose of the tests was to obtain overall performance and influencing factors as well as detail...
A low speed wind tunnel test was conducted in the Langley V/STOL tunnel to determine the static long...