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On the Scaling Laws and Similarity Spectra for Jet Noise in Subsonic and Supersonic Flow
Author(s) -
Max Kandula
Publication year - 2008
Publication title -
the international journal of acoustics and vibration
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.232
H-Index - 19
eISSN - 2415-1408
pISSN - 1027-5851
DOI - 10.20855/ijav.2008.13.1220
Subject(s) - jet noise , supersonic speed , jet (fluid) , similarity (geometry) , noise (video) , physics , scaling law , flow (mathematics) , scaling , mechanics , spectral line , choked flow , acoustics , mathematics , computer science , geometry , astronomy , artificial intelligence , image (mathematics)
The scaling laws for the simulation of noise from subsonic and ideally expanded supersonic jets are reviewed with regard to their applicability to deduce full-scale conditions from small-scale model testing. Important parameters of scale model testing for the simulation of jet noise are identified, and the methods of estimating full- scale noise levels from simulated scale model data are addressed. The limitations of cold-jet data in estimating high-temperature supersonic jet noise levels are discussed. New results are presented showing the dependence of overall sound power level on the jet temperature ratio at various jet Mach numbers. A generalized similarity spectrum is also proposed, which accounts for convective Mach number and angle to the jet axis.

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