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Reflection and Refraction of Acoustic Waves by a Shock WaveThe presence of sound waves in one or the other of the fluid regions on either side of a shock wave is made apparent, in the region under superpressure, by acoustic waves (reflected or refracted according to whether the incident waves lie in the region of superpressure or of subpressure) and by thermal waves. The characteristics of these waves are calculated for a plane, progressive, and uniform incident wave. In the case of refraction, the refracted acoustic wave can, according to the incidence, be plane, progressive, and uniform or take the form of an 'accompanying wave' which remains attached to the front of the shock while sliding parallel to it. In all cases, geometrical constructions permit determination of the kinematic characteristics of the reflected or refractive acoustic waves. The dynamic relationships show that the amplitude of the reflected wave is always less than that of the incident wave. The amplitude of the refracted wave, whatever its type, may in certain cases be greater than that of the incident wave.
Document ID
20040034183
Acquisition Source
Headquarters
Document Type
Other - NACA Technical Memorandum
Authors
Brillouin, J.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 1957
Publication Information
Publication: Reflexion et Refraction d'ondes Acoustiques Par Une Onde de Choc
Volume: 5
Issue: 3
Subject Category
Acoustics
Report/Patent Number
NACA-TM-1409
Report Number: NACA-TM-1409
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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