The Tiltrotor Test Rig (TTR) provides new proprotor testing capabilities to the National Aeronautics and Space Administration (NASA) and the Department of Defense (DoD). A checkout test for the TTR with the 699 proprotor was performed in the National Full-Scale Aerodynamics Complex (NFAC) 40- by 80 Foot Wind Tunnel from 2017 to 2018. Four microphones were placed around the rotor to capture acoustic data. Revolution based acoustic data processing techniques are evaluated for appropriateness in both helicopter and airplane configurations. This paper presents the acoustic data acquired for the rotor in conversion and airplane configuration
A 2.1 m diameter, 1/6-scale model helicopter main rotor was tested in hover in the test section of t...
Acoustic measurements were obtained in a Langley 14 x 22 foot Subsonic Wind Tunnel to study the aero...
A 2.1-m diam., 1/6-scale model helicopter main rotor was tested in hover in the test section of the ...
The Tiltrotor Test Rig (TTR) was tested in the National Full-Scale Aerodynamics Complex (NFAC) 40- b...
The Tiltrotor Test Rig (TTR) with the Bell 699 Rotor was tested in the National Full-Scale Aerodynam...
The Tiltrotor Test Rig (TTR) is a new NASA facility for testing full-scale proprotors. The first tes...
The Tiltrotor Test Rig (TTR) is a NASA project, joint with the U.S. Army and Air Force, to develop a...
The NASA Tiltrotor Test Rig (TTR) is a new, large-scale proprotor test system, developed jointly wit...
A full-scale isolated proprotor test was recently conducted in the USAF National Full-Scale Aerodyna...
In 2018, a full-scale isolated proprotor test was conducted in the USAF National Full-Scale Aerodyna...
The unique capabilities of the National Full-Scale Aerodynamics Complex (NFAC) for testing rotorcraf...
The prediction of the performance and loads of a full-scale isolated proprotor and the calculation o...
An investigation of helicopter rotor noise at model scale was conducted in the Langley 4 by 7 meter ...
An aeroacoustic wind tunnel test was conducted using a scaled isolated tiltrotor model. Acoustic dat...
A cooperative flight test by NASA, Bell Helicopter and the U.S. Army to characterize the steady stat...
A 2.1 m diameter, 1/6-scale model helicopter main rotor was tested in hover in the test section of t...
Acoustic measurements were obtained in a Langley 14 x 22 foot Subsonic Wind Tunnel to study the aero...
A 2.1-m diam., 1/6-scale model helicopter main rotor was tested in hover in the test section of the ...
The Tiltrotor Test Rig (TTR) was tested in the National Full-Scale Aerodynamics Complex (NFAC) 40- b...
The Tiltrotor Test Rig (TTR) with the Bell 699 Rotor was tested in the National Full-Scale Aerodynam...
The Tiltrotor Test Rig (TTR) is a new NASA facility for testing full-scale proprotors. The first tes...
The Tiltrotor Test Rig (TTR) is a NASA project, joint with the U.S. Army and Air Force, to develop a...
The NASA Tiltrotor Test Rig (TTR) is a new, large-scale proprotor test system, developed jointly wit...
A full-scale isolated proprotor test was recently conducted in the USAF National Full-Scale Aerodyna...
In 2018, a full-scale isolated proprotor test was conducted in the USAF National Full-Scale Aerodyna...
The unique capabilities of the National Full-Scale Aerodynamics Complex (NFAC) for testing rotorcraf...
The prediction of the performance and loads of a full-scale isolated proprotor and the calculation o...
An investigation of helicopter rotor noise at model scale was conducted in the Langley 4 by 7 meter ...
An aeroacoustic wind tunnel test was conducted using a scaled isolated tiltrotor model. Acoustic dat...
A cooperative flight test by NASA, Bell Helicopter and the U.S. Army to characterize the steady stat...
A 2.1 m diameter, 1/6-scale model helicopter main rotor was tested in hover in the test section of t...
Acoustic measurements were obtained in a Langley 14 x 22 foot Subsonic Wind Tunnel to study the aero...
A 2.1-m diam., 1/6-scale model helicopter main rotor was tested in hover in the test section of the ...