Simultaneous Vibration and Noise Reduction in Rotorcraft - Practical Implementation Issues
- 18 April 2005
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 17 references indexed in Scilit:
- Rotary-Wing Aeroelasticity: Current Status and Future TrendsAIAA Journal, 2004
- Reduction of Vibrations due to Dynamic Stall in Helicopters using an Actively Controlled FlapPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2002
- New developments in vibration reduction with actively controlled trailing edge flapsMathematical and Computer Modelling, 2001
- Application of a New Compressible Time Domain Aerodynamic Model to Vibration Reduction in Helicopters Using an Actively Controlled FlapJournal of the American Helicopter Society, 2001
- Rotor blade–vortex interaction noiseProgress in Aerospace Sciences, 2000
- Key Results From a Higher Harmonic Control Aeroacoustic Rotor Test (HART)Journal of the American Helicopter Society, 1997
- Vibration reduction in rotorcraft using active control - A comparison of various approachesJournal of Guidance, Control, and Dynamics, 1995
- A Higher Harmonic Control Test in the DNW to Reduce Impulsive BVI NoiseJournal of the American Helicopter Society, 1994
- The Effects of Higher Harmonic Control on Blade-Vortex Interaction Noise and VibrationJournal of the American Helicopter Society, 1993
- Technical Notes: Reduction of Blade‐Vortex Interaction Noise Through Higher Harmonic Pitch ControlJournal of the American Helicopter Society, 1990