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Reynolds stress closure in jet flows using wave modelsA collection of papers is presented. The outline of this report is as follows. Chapter three contains a description of a weakly nonlinear turbulence model that was developed. An essential part of the application of such a closure scheme to general geometry jets is the solution of the local hydrodynamic stability equation for a given jet cross-section. Chapter four describes the conformal mapping schemes used to map such geometries onto a simple computational domain. Chapter five describes a solution of a stability problem for circular, elliptic, and rectangular geometries. In chapter six linear models for the shock shell structure in non-circular jets is given. The appendices contain reprints of papers also published during this study including the following topics: (1) instability of elliptic jets; (2) a technique for predicting the shock cell structure in non-circular jets using a vortex sheet model; and (3) the resonant interaction between twin supersonic jets.
Document ID
19910004327
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Morris, Philip J.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1990
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-185717
NAS 1.26:185717
Report Number: NASA-CR-185717
Report Number: NAS 1.26:185717
Accession Number
91N13640
Funding Number(s)
CONTRACT_GRANT: NAG1-657
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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