Effects of Jet Temperature and Nozzle-Lip Thickness on Screech Tones
- 1 May 2000
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 38 (5) , 762-767
- https://doi.org/10.2514/2.1055
Abstract
No abstract availableThis publication has 19 references indexed in Scilit:
- Numerical Simulation of the Generation of Axisymmetric Mode Jet Screech TonesAIAA Journal, 1998
- Flow/acoustic coupling in ducted jetsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Advances in understanding supersonic jet screechPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Flight Effects on the Far-Field Noise of a Heated Supersonic JetAIAA Journal, 1997
- Screech frequency prediction in light of mode detection and convection speed measurements for heated jetsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Supersonic Jet NoiseAnnual Review of Fluid Mechanics, 1995
- Screech tones from free and ducted supersonic jetsAIAA Journal, 1994
- Proposed relationship between broadband shock associated noise and screech tonesJournal of Sound and Vibration, 1986
- Recent observations including temperature dependence of axisymmetricjet screechAIAA Journal, 1975
- On the Mechanism of Choked Jet NoiseProceedings of the Physical Society. Section B, 1953