Three-Dimensional Numerical Simulation of the Jet Screech Phenomenon
- 1 January 2002
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 40 (1) , 33-41
- https://doi.org/10.2514/2.1638
Abstract
No abstract availableKeywords
This publication has 22 references indexed in Scilit:
- Effects of Jet Temperature and Nozzle-Lip Thickness on Screech TonesAIAA Journal, 2000
- Numerical Simulation of the Generation of Axisymmetric Mode Jet Screech TonesAIAA Journal, 1998
- Screech Tones of Supersonic Jets from Bevelled Rectangular NozzlesAIAA Journal, 1997
- The effects of nozzle exit lip thickness on plume resonanceJournal of Sound and Vibration, 1992
- Theoretical model of discrete tone generation by impinging jetsJournal of Fluid Mechanics, 1990
- On the three families of instability waves of high-speed jetsJournal of Fluid Mechanics, 1989
- Proposed relationship between broadband shock associated noise and screech tonesJournal of Sound and Vibration, 1986
- Screech suppression in supersonic jetsAIAA Journal, 1983
- Shock associated noise of supersonic jets from convergent-divergent nozzlesJournal of Sound and Vibration, 1982
- On the Mechanism of Choked Jet NoiseProceedings of the Physical Society. Section B, 1953