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Wave equations and computational models for sonic boom propagation through a turbulent atmosphereThe improved simulation of sonic boom propagation through the real atmosphere requires greater understanding of how the transient acoustic pulses popularly termed sonic booms are affected by atmospheric turbulence. A nonlinear partial differential equation that can be used to simulate the effects of smaller-scale atmospheric turbulence on sonic boom waveforms is described. The equation is first order in the time derivative and involves an extension of geometrical acoustics to include diffraction phenomena. Various terms in the equation are explained in physical terms. Such terms include those representing convection at the wave speed, diffraction, molecular relaxation, classical dissipation, and nonlinear steepening. The atmospheric turbulence enters through an effective sound speed, which varies with all three spatial coordinates, and which is the sum of the local sound speed and the component of the turbulent flow velocity projected along a central ray that connects the aircraft trajectory with the listener.
Document ID
19920024633
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pierce, Allan D.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Publication Information
Publication: NASA. Langley Research Center, High-Speed Research: Sonic Boom, Volume 1
Subject Category
Acoustics
Accession Number
92N33877
Funding Number(s)
CONTRACT_GRANT: NAG1-947
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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