Flight-Path Management/Control Methodology to Reduce Helicopter Blade-Vortex Interaction Noise
- 1 March 2002
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 39 (2) , 193-205
- https://doi.org/10.2514/2.2923
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Noise prediction for maneuvering rotorcraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- Operational Tests of Noise Abatement Approaches for Rotorcraft Using Differential GPS for GuidanceJournal of the American Helicopter Society, 1998
- Prediction and Measurement of Blade - Vortex InteractionJournal of Aircraft, 1998
- Reduction of Blade-Vortex Interaction (BVI) Noise through X-Force ControlJournal of the American Helicopter Society, 1998
- FOCUSING OF HELICOPTER BVI NOISEJournal of Sound and Vibration, 1996
- Linear Acoustic Formulas for Calculation of Rotating Blade NoiseAIAA Journal, 1981
- Helicopter Noise: State-of-the-ArtJournal of Aircraft, 1978
- Reduction of VTOL Operational Noise through Flight Trajectory ManagementJournal of Aircraft, 1973
- Sound generation by turbulence and surfaces in arbitrary motionPhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1969
- The sound field for singularities in motionProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1965