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COMOC: Three dimensional boundary region variant, programmer's manualThe three-dimensional boundary region variant of the COMOC computer program system solves the partial differential equation system governing certain three-dimensional flows of a viscous, heat conducting, multiple-species, compressible fluid including combustion. The solution is established in physical variables, using a finite element algorithm for the boundary value portion of the problem description in combination with an explicit marching technique for the initial value character. The computational lattice may be arbitrarily nonregular, and boundary condition constraints are readily applied. The theoretical foundation of the algorithm, a detailed description on the construction and operation of the program, and instructions on utilization of the many features of the code are presented.
Document ID
19750024311
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Orzechowski, J. A.
(Bell Aerospace Co. Buffalo, NY, United States)
Baker, A. J.
(Bell Aerospace Co. Buffalo, NY, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1974
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-132449
D9192-954001
Report Number: NASA-CR-132449
Report Number: D9192-954001
Accession Number
75N32384
Funding Number(s)
CONTRACT_GRANT: NAS1-11214
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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