A parallel three-dimensional computational aeroacoustics method using non-linear disturbance equations
- 6 May 1996
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Toward the direct calculation of noise - Fluid/acoustic coupled simulationAIAA Journal, 1995
- Structure of supersonic jet flow and its radiated soundAIAA Journal, 1994
- Sound generated by instability waves of supersonic flows. Part 2. Axisymmetric jetsJournal of Fluid Mechanics, 1984
- Far field boundary conditions for compressible flowsJournal of Computational Physics, 1982
- Experiments on the flow and acoustic properties of a moderate-Reynolds-number supersonic jetJournal of Fluid Mechanics, 1982
- On the Radiation of Sound by the Instability Waves of a Compressible Axisymmetric JetPublished by Springer Nature ,1979
- On sound generated aerodynamically I. General theoryProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1952