Add to ORKGA hover test of a full-scale 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 the original, metal-blade XV-15 rotor system. Data were acquired for rotor tip Mach numbers ranging from 0.60 to 0.73. This report presents data on rotor performance, rotor wake downwash velocities, and rotor loads
Two rotor systems for the UH-1 helicopter were tested in hover and forward flight. The baseline syst...
The performance of a full-scale XV-15 rotor operating in low-speed helicopter-mode flight on a rotor...
An analysis of the rotor and control system loads of the XV-15 with the Advanced Technology Blades (...
A hover test of a full-scale, composite, advanced technology XV-15 rotor was conducted at the Outdoo...
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...
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...
The XV-15 aircraft was tested in the Ames 40 by 80 Foot Wind Tunnel for preliminary evaluation of ae...
An experiment has been performed to investigate the far-field hover acoustic characteristics of the ...
The Tiltrotor Test Rig (TTR) is a new NASA facility for testing full-scale proprotors. The first tes...
A fleet of civil tilt rotor transports offers a means of reducing airport congestion and point-to-po...
An experimental and theoretical investigation of rotor/wing aerodynamic interactions in hover is des...
Two rotor systems for the UH-1 helicopter were tested in hover and forward flight. The baseline syst...
The performance of a full-scale XV-15 rotor operating in low-speed helicopter-mode flight on a rotor...
An analysis of the rotor and control system loads of the XV-15 with the Advanced Technology Blades (...
A hover test of a full-scale, composite, advanced technology XV-15 rotor was conducted at the Outdoo...
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...
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...
The XV-15 aircraft was tested in the Ames 40 by 80 Foot Wind Tunnel for preliminary evaluation of ae...
An experiment has been performed to investigate the far-field hover acoustic characteristics of the ...
The Tiltrotor Test Rig (TTR) is a new NASA facility for testing full-scale proprotors. The first tes...
A fleet of civil tilt rotor transports offers a means of reducing airport congestion and point-to-po...
An experimental and theoretical investigation of rotor/wing aerodynamic interactions in hover is des...
Two rotor systems for the UH-1 helicopter were tested in hover and forward flight. The baseline syst...
The performance of a full-scale XV-15 rotor operating in low-speed helicopter-mode flight on a rotor...
An analysis of the rotor and control system loads of the XV-15 with the Advanced Technology Blades (...