Study of the noise mechanisms of transonic blade-vortex interactions
- 1 October 1991
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 29 (10), 1562-1572
- https://doi.org/10.2514/3.10776
Abstract
No abstract availableThis publication has 21 references indexed in Scilit:
- Blade-vortex interactionAIAA Journal, 1989
- Helicopter Impulsive Noise: Theoretical and Experimental StatusPublished by Springer Nature ,1986
- Second-order-accurate spatial differencing for the transonic small-disturbance equationAIAA Journal, 1985
- Monotone switches in implicit algorithms for potential equations applied to transonic flowsAIAA Journal, 1985
- Flow field and acoustics of two-dimensional transonic blade-vortex interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Interactions of airfoils with gusts and concentrated vortices in unsteady transonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Rotor-vortex interaction noisePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Effect of Frequency in Unsteady Transonic FlowAIAA Journal, 1979
- Helicopter Noise: State-of-the-ArtJournal of Aircraft, 1978
- Implicit Finite-Difference Computations of Unsteady Transonic Flows about AirfoilsAIAA Journal, 1977