Numerical and Asymptotic Lilley-Equation Solutions for the Goldstein Jet-Noise Source Model

Author:

Morfey Christopher1,Tester Brian1,Powles Christopher1

Affiliation:

1. ISVR

Publisher

American Institute of Aeronautics and Astronautics

Reference10 articles.

1. 1Morris,P.J.,andBoluriaan,S."ThePredictionofJetNoisefromCFDData,"AIAA2004-2977,2004.

2. Modelling of fine-scale turbulence mixing noise

3. 3Goldstein,M.E.,andKhavaran,A."AcousticSourceModelingforHigh-SpeedAirJets,"AIAA2005-0415,2005.

4. 4Bassetti,A.,andMorfey,C.L."AnAcousticAnalogyModelforJetNoisePrediction,"AIAA2007-3642,2007.

5. An exact form of Lilley's equation with a velocity quadrupole/temperature dipole source term

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1. Numerical Study on Flow and Noise Characteristics of High-Temperature and High-Pressure Steam Ejector;Energies;2023-05-17

2. Asymptotic and Numerical Solutions for Shielding of Noise Sources by Parallel Coaxial Jet Flows;14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference);2008-05-05

3. An Acoustic-Analogy Model for Jet-Noise Prediction;13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference);2007-05-21

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