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A comparative study of two codes with an improved two-equation turbulence model for predicting jet plumesCompressible jet plumes were studied using a two-equation turbulence model. A space marching procedure based on an upwind numerical scheme was used to solve the governing equations and turbulence transport equations. The computed results indicate that extending the space marching procedure for solving supersonic/subsonic mixing problems can be stable, efficient and accurate. Moreover, a newly developed correction for compressible dissipation has been verified in fully expanded and underexpanded jet plumes. For a sonic jet plume, no improvement in results over the standard two-equation model was seen. However for a supersonic jet plume, the correction due to compressible dissipation successfully predicted the reduced spreading rate of the jet compared to the sonic case. The computed results were generally in good agreement with the experimental data.
Document ID
19920062857
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Balakrishnan, L.
(Old Dominion University, Norfolk; NASA, Langley Research Center Hampton, VA, United States)
Abdol-Hamid, Khaled S.
(Analytical Services and Materials, Inc.; NASA, Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 92-2604
Meeting Information
Meeting: AIAA Applied Aerodynamics Conference
Location: Palo Alto, CA
Country: United States
Start Date: June 22, 1992
End Date: June 24, 1992
Accession Number
92A45481
Distribution Limits
Public
Copyright
Other

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