Add to ORKGA hover test of a full-scale, composite, advanced technology XV-15 rotor was conducted at the Outdoor Aerodynamic Research Facility at Ames Research Center. The primary objective of the test was to obtain accurate measurements of the hover performance of this rotor system. Data were acquired for rotor tip Mach numbers ranging from 0.35 to 0.73. The rotor was tested with several alternate blade root and blade-tip configurations. Data are presented on rotor performance, rotor-wake downwash velocities, and rotor system loads
An experiment has been performed to investigate the far-field hover acoustic characteristics of the ...
An investigation was conducted in the Langley Transonic Dynamics Tunnel to obtain data to permit eva...
The Tiltrotor Test Rig (TTR) is a new NASA facility for testing full-scale proprotors. The first tes...
A hover test of a full-scale XV-15 rotor was conducted at the Outdoor Aerodynamic Research Facility ...
A hover test of a 0.658-scale model of a V-22 rotor and wing was conducted at the Outdoor Aerodynami...
Rotor hover performance data were obtained for two full-scale rotor systems designed for the XV-15 T...
Rotor hover-performance data from a 1/6-scale helicopter rotor are analyzed and the data sets compar...
Two rotor systems for the UH-1 helicopter were tested in hover and forward flight. The baseline syst...
The design features and general characteristics of the NASA/Army XV-15 tilt rotor research aircraft ...
A full-scale isolated proprotor test was recently conducted in the USAF National Full-Scale Aerodyna...
The design characteristics of the XV-15 Tilt rotor research aircraft are presented. Particular atten...
An analysis of the rotor and control system loads of the XV-15 with the Advanced Technology Blades (...
Comparisons were made of the performance and blade vibratory loads characteristics for an advanced r...
The XV-15 aircraft was tested in the Ames 40 by 80 Foot Wind Tunnel for preliminary evaluation of ae...
A test of a small scale 3-bladed model rotor, with these test results with predictions using a rotor...
An experiment has been performed to investigate the far-field hover acoustic characteristics of the ...
An investigation was conducted in the Langley Transonic Dynamics Tunnel to obtain data to permit eva...
The Tiltrotor Test Rig (TTR) is a new NASA facility for testing full-scale proprotors. The first tes...
A hover test of a full-scale XV-15 rotor was conducted at the Outdoor Aerodynamic Research Facility ...
A hover test of a 0.658-scale model of a V-22 rotor and wing was conducted at the Outdoor Aerodynami...
Rotor hover performance data were obtained for two full-scale rotor systems designed for the XV-15 T...
Rotor hover-performance data from a 1/6-scale helicopter rotor are analyzed and the data sets compar...
Two rotor systems for the UH-1 helicopter were tested in hover and forward flight. The baseline syst...
The design features and general characteristics of the NASA/Army XV-15 tilt rotor research aircraft ...
A full-scale isolated proprotor test was recently conducted in the USAF National Full-Scale Aerodyna...
The design characteristics of the XV-15 Tilt rotor research aircraft are presented. Particular atten...
An analysis of the rotor and control system loads of the XV-15 with the Advanced Technology Blades (...
Comparisons were made of the performance and blade vibratory loads characteristics for an advanced r...
The XV-15 aircraft was tested in the Ames 40 by 80 Foot Wind Tunnel for preliminary evaluation of ae...
A test of a small scale 3-bladed model rotor, with these test results with predictions using a rotor...
An experiment has been performed to investigate the far-field hover acoustic characteristics of the ...
An investigation was conducted in the Langley Transonic Dynamics Tunnel to obtain data to permit eva...
The Tiltrotor Test Rig (TTR) is a new NASA facility for testing full-scale proprotors. The first tes...