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A Study of Fundamental Shock Noise MechanismsThis paper investigates two mechanisms fundamental to sound generation in shocked flows: shock motion and shock deformation. Shock motion is modeled numerically by examining the interaction of a sound wave with a shock. This numerical approach is validated by comparison with results obtained by linear theory for a small-disturbance case. Analysis of the perturbation energy with Myers' energy corollary demonstrates that acoustic energy is generated by the interaction of acoustic disturbances with shocks. This analysis suggests that shock motion generates acoustic and entropy disturbance energy. Shock deformation is modeled numerically by examining the interaction of a vortex ring with a shock. These numerical simulations demonstrate the generation of both an acoustic wave and contact surfaces. The acoustic wave spreads cylindrically. The sound intensity is highly directional and the sound pressure increases with increasing shock strength. The numerically determined relationship between the sound pressure and the Mach number is found to be consistent with experimental observations of shock noise. This consistency implies that a dominant physical process in the generation of shock noise is modeled in this study.
Document ID
19970022251
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Meadows, Kristine R.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1997
Subject Category
Acoustics
Report/Patent Number
NASA-TP-3605
NAS 1.60:3605
L-17530
Report Number: NASA-TP-3605
Report Number: NAS 1.60:3605
Report Number: L-17530
Accession Number
97N22825
Funding Number(s)
PROJECT: RTOP 505-59-52-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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