https://doi.org/10.21949/14034721994PDFTech ReportWind tunnelsRotorsMechanical propertiesAerodynamicsPerformanceLSDRLarge Scale Dynamic RigMDART rotorMcDonnell Douglas Advanced Rotor TechnologyShake testNguyen, KhanhLau, BentonAmes Research CenterNTL-AVIATION-Aviation Safety/AirworthinessUS Transportation CollectionA shake test was performed on the Large Scale Dynamic Rig in the 40- by 80-Foot Wind Tunnel in support of the McDonnell Douglas Advanced Rotor Technology (MDART) Test Program. The shake test identifies the hub modes and the dynamic calibration matrix of the rotor balance. For hub mode identification, three configurations were tested: wind tunnel scale unlocked with dampers engaged and disengaged, and wind tunnel scale locked. Te...
The objective of this investigation is to illustrate the steps involved in developing a multibody dy...
A wind-tunnel investigation of tiltrotor whirl-flutter stability boundaries has been conducted on a ...
Modal parameters such as resonance frequencies, damping ratios, and mode shapes of aircraft prototyp...
Prior to the full-scale wind tunnel test of the UH-60A Airloads rotor, a shake test was completed on...
A shake test was conducted in the 80- by 120-Foot Wind Tunnel at NASA Ames Research Center, using th...
A shake test was conducted to determine the dynamic characteristics of a rotor test apparatus on str...
An advanced rotor and propeller rig for tip Mach-scaled wind tunnel testing is the subject of dynami...
The Tiltrotor Test Rig (TTR) is being developed at the NASA Ames Research Center for testing full-sc...
The NASA Ames Rotor Test Apparatus was modified to include a Steady/Dynamic Rotor Balance. The dynam...
This paper presents the results from an ongoing effort to produce improved correlation between analy...
A heavily instrumented 1:5 scaled model of the ERICA tilt-wing configuration has been tested in the ...
A shake test was conducted to determine the dynamic characteristics of a propeller test rig in the A...
A method is described for measuring the dynamic stability derivatives of a model airplane in a wind ...
Tiltrotor aircraft encounter an aeroelastic instability called whirl flutter at high speeds. Whirl f...
A mathematical model is developed for the dynamics of a wind tunnel support system consisting of a b...
The objective of this investigation is to illustrate the steps involved in developing a multibody dy...
A wind-tunnel investigation of tiltrotor whirl-flutter stability boundaries has been conducted on a ...
Modal parameters such as resonance frequencies, damping ratios, and mode shapes of aircraft prototyp...
Prior to the full-scale wind tunnel test of the UH-60A Airloads rotor, a shake test was completed on...
A shake test was conducted in the 80- by 120-Foot Wind Tunnel at NASA Ames Research Center, using th...
A shake test was conducted to determine the dynamic characteristics of a rotor test apparatus on str...
An advanced rotor and propeller rig for tip Mach-scaled wind tunnel testing is the subject of dynami...
The Tiltrotor Test Rig (TTR) is being developed at the NASA Ames Research Center for testing full-sc...
The NASA Ames Rotor Test Apparatus was modified to include a Steady/Dynamic Rotor Balance. The dynam...
This paper presents the results from an ongoing effort to produce improved correlation between analy...
A heavily instrumented 1:5 scaled model of the ERICA tilt-wing configuration has been tested in the ...
A shake test was conducted to determine the dynamic characteristics of a propeller test rig in the A...
A method is described for measuring the dynamic stability derivatives of a model airplane in a wind ...
Tiltrotor aircraft encounter an aeroelastic instability called whirl flutter at high speeds. Whirl f...
A mathematical model is developed for the dynamics of a wind tunnel support system consisting of a b...
The objective of this investigation is to illustrate the steps involved in developing a multibody dy...
A wind-tunnel investigation of tiltrotor whirl-flutter stability boundaries has been conducted on a ...
Modal parameters such as resonance frequencies, damping ratios, and mode shapes of aircraft prototyp...