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CFD code evaluation for internal flow modelingResearch on the computational fluid dynamics (CFD) code evaluation with emphasis on supercomputing in reacting flows is discussed. Advantages of unstructured grids, multigrids, adaptive methods, improved flow solvers, vector processing, parallel processing, and reduction of memory requirements are discussed. As examples, researchers include applications of supercomputing to reacting flow Navier-Stokes equations including shock waves and turbulence and combustion instability problems associated with solid and liquid propellants. Evaluation of codes developed by other organizations are not included. Instead, the basic criteria for accuracy and efficiency have been established, and some applications on rocket combustion have been made. Research toward an ultimate goal, the most accurate and efficient CFD code, is in progress and will continue for years to come.
Document ID
19910005244
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chung, T. J.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1990
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-187677
NAS 1.26:187677
Report Number: NASA-CR-187677
Report Number: NAS 1.26:187677
Accession Number
91N14557
Funding Number(s)
CONTRACT_GRANT: NAG8-95
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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