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Investigation to define the propagation characteristics of a finite amplitude acoustic pressure waveA theoretical analysis of the propagation characteristics of a finite amplitude pressure wave is presented. The analysis attempts to study the contribution of entropy-producing regions to the mechanism of aerodynamic noise generation. It results in a nonlinear convective wave equation in terms of entropy and a thermodynamic 'J' function. A direct analogy between the derived governing equation and those used in classical literature is obtained. An idealization of the processes considered permits the uncoupling of the equations of motion with a consequent construction of an acoustic analogy treating shock wave emission of finite amplitude acoustic waves. An engineering approach is reflected in the concept of an extended plug nozzle whose function is to facilitate aerodynamic noise attenuation by modifying the entropy-producing regions.
Document ID
19670012652
Acquisition Source
Marshall Space Flight Center
Document Type
Contractor Report (CR)
Authors
Peter, A. C.
(North American Aviation, Inc. Downey, CA, United States)
Cottrell, J. W.
(North American Aviation, Inc. Downey, CA, United States)
Date Acquired
August 3, 2013
Publication Date
April 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-736
Report Number: NASA-CR-736
Accession Number
67N21981
Funding Number(s)
CONTRACT_GRANT: NAS8-11441
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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