Add to ORKGBackground information is presented for the helicopter rotor test facility, in preface to a more detailed discussion of major subsystems equipment, including error considerations, frequency response, and display instrumentation
The Tiltrotor Test Rig (TTR) provides new proprotor testing capabilities to the National Aeronautics...
For over half a century the NPS Aerolabʼ Low Speed Wind Tunnel located in Halligan Hall of the Nava...
The flight test activities of the Rotor System Research Aircraft (RSRA), NASA 740, from June 30, 198...
The configuration, operation and maintenance requirements for the contractor-furnished portion of th...
An investigation of helicopter rotor noise at model scale was conducted in the Langley 4 by 7 meter ...
A small-scale powered rotor model was designed for use as a research tool in the exploratory testing...
A rotor hover test was performed inside the JPL 25-foot-diameter Space Simulator. The 40-inch-diamet...
The Tiltrotor Test Rig (TTR) with the Bell 699 Rotor was tested in the National Full-Scale Aerodynam...
Pilot rating comments and standard deviation measures of flight performance and control use are pres...
The unique capabilities of the National Full-Scale Aerodynamics Complex (NFAC) for testing rotorcraf...
Rotor hover-performance data from a 1/6-scale helicopter rotor are analyzed and the data sets compar...
A ground-simulation experiment was conducted to investigate the influence and interaction of flight-...
A test program was conducted to isolate and evaluate the individual noise sources of a light helicop...
Information processing demands on both civilian and military aircrews have increased enormously as r...
Comparisons were made of the performance and blade vibratory loads characteristics for an advanced r...
The Tiltrotor Test Rig (TTR) provides new proprotor testing capabilities to the National Aeronautics...
For over half a century the NPS Aerolabʼ Low Speed Wind Tunnel located in Halligan Hall of the Nava...
The flight test activities of the Rotor System Research Aircraft (RSRA), NASA 740, from June 30, 198...
The configuration, operation and maintenance requirements for the contractor-furnished portion of th...
An investigation of helicopter rotor noise at model scale was conducted in the Langley 4 by 7 meter ...
A small-scale powered rotor model was designed for use as a research tool in the exploratory testing...
A rotor hover test was performed inside the JPL 25-foot-diameter Space Simulator. The 40-inch-diamet...
The Tiltrotor Test Rig (TTR) with the Bell 699 Rotor was tested in the National Full-Scale Aerodynam...
Pilot rating comments and standard deviation measures of flight performance and control use are pres...
The unique capabilities of the National Full-Scale Aerodynamics Complex (NFAC) for testing rotorcraf...
Rotor hover-performance data from a 1/6-scale helicopter rotor are analyzed and the data sets compar...
A ground-simulation experiment was conducted to investigate the influence and interaction of flight-...
A test program was conducted to isolate and evaluate the individual noise sources of a light helicop...
Information processing demands on both civilian and military aircrews have increased enormously as r...
Comparisons were made of the performance and blade vibratory loads characteristics for an advanced r...
The Tiltrotor Test Rig (TTR) provides new proprotor testing capabilities to the National Aeronautics...
For over half a century the NPS Aerolabʼ Low Speed Wind Tunnel located in Halligan Hall of the Nava...
The flight test activities of the Rotor System Research Aircraft (RSRA), NASA 740, from June 30, 198...