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Nonequilibrium chemistry boundary layer integral matrix procedureThe development of an analytic procedure for the calculation of nonequilibrium boundary layer flows over surfaces of arbitrary catalycities is described. An existing equilibrium boundary layer integral matrix code was extended to include nonequilibrium chemistry while retaining all of the general boundary condition features built into the original code. For particular application to the pitch-plane of shuttle type vehicles, an approximate procedure was developed to estimate the nonequilibrium and nonisentropic state at the edge of the boundary layer.
Document ID
19730023103
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tong, H.
(Acurex Corp. Mountain View, CA, United States)
Buckingham, A. C.
(Acurex Corp. Mountain View, CA, United States)
Morse, H. L.
(Acurex Corp. Mountain View, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1973
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AEROTHERM-73-67
REPT-73-67
NASA-CR-134039
Report Number: AEROTHERM-73-67
Report Number: REPT-73-67
Report Number: NASA-CR-134039
Accession Number
73N31835
Funding Number(s)
PROJECT: AEROTHERM PROJ. 6099
CONTRACT_GRANT: NAS9-9494
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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