A prediction of high-speed rotor noise
- 10 April 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Geometrical acoustics and transonic helicopter soundPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Conservative full-potential model for unsteady transonic rotor flowsAIAA Journal, 1987
- Solution of transonic flow past rotor blades using the conservative full potential equationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Numerical solution of the full-potential equation for rotors and oblique wings using a new wake modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985