A Study of Rotorcraft Noise Prediction in Maneuvering Flight
- 5 January 2004
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Flight-Path Management/Control Methodology to Reduce Helicopter Blade-Vortex Interaction NoiseJournal of Aircraft, 2002
- Blade‐Vortex Interaction Data Obtained from a Pressure‐Instrumented Model UH‐60A Rotor at the DNWJournal of the American Helicopter Society, 1993
- Acoustic Predictions Using Measured Pressures from a Model Rotor in the DNWJournal of the American Helicopter Society, 1993