Add to ORKGThis presentation gives insight into a joint flight testing effort that included participation from ...
The Terminal Area Productivity (TAP) research program was initiated by NASA to increase the airport ...
A full scale inlet test was to be done in the NASA-ARC 40' X 80' WT to demonstrate satisfactory inle...
An aircraft system noise assessment was performed for the hybrid wing body aircraft concept, known a...
NASAs Environmentally Responsible Aviation (ERA) Project explores enabling technologies to reduce av...
For the NASA X-56a Program, Armstrong Flight Research Center has been developing a set of linear sta...
Simulation data are reported for the purpose of programming the flight simulator for advanced aircra...
The effects of inlet turbulence intensity on the aerodynamic performance of a variable speed power t...
Information is given in graphical and outline form on a pilot/vehicle model description, control of ...
Comparison of theoretical and simulated low speed landing characteristics for large transport aircra...
On-board estimation, navigation and control technologies addressing safety problems of robotic fligh...
A wind tunnel investigation, employing a 1/8 scale model in an 11 foot transonic wind tunnel (Mach 0...
Flying cars have nearly mythical appeal to nonpilots, a group that includes almost the whole human r...
Cruise scene visual attachment system assembly and detail design drawings for manned spacecraft or a...
Propulsion integration for low-boom supersonic aircraft requires careful inlet selection, placement,...
This presentation gives insight into a joint flight testing effort that included participation from ...
The Terminal Area Productivity (TAP) research program was initiated by NASA to increase the airport ...
A full scale inlet test was to be done in the NASA-ARC 40' X 80' WT to demonstrate satisfactory inle...
An aircraft system noise assessment was performed for the hybrid wing body aircraft concept, known a...
NASAs Environmentally Responsible Aviation (ERA) Project explores enabling technologies to reduce av...
For the NASA X-56a Program, Armstrong Flight Research Center has been developing a set of linear sta...
Simulation data are reported for the purpose of programming the flight simulator for advanced aircra...
The effects of inlet turbulence intensity on the aerodynamic performance of a variable speed power t...
Information is given in graphical and outline form on a pilot/vehicle model description, control of ...
Comparison of theoretical and simulated low speed landing characteristics for large transport aircra...
On-board estimation, navigation and control technologies addressing safety problems of robotic fligh...
A wind tunnel investigation, employing a 1/8 scale model in an 11 foot transonic wind tunnel (Mach 0...
Flying cars have nearly mythical appeal to nonpilots, a group that includes almost the whole human r...
Cruise scene visual attachment system assembly and detail design drawings for manned spacecraft or a...
Propulsion integration for low-boom supersonic aircraft requires careful inlet selection, placement,...
This presentation gives insight into a joint flight testing effort that included participation from ...
The Terminal Area Productivity (TAP) research program was initiated by NASA to increase the airport ...
A full scale inlet test was to be done in the NASA-ARC 40' X 80' WT to demonstrate satisfactory inle...