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Ablation and radiation coupled viscous hypersonic shock layers, volume 1The results for a stagnation-line analysis of the radiative heating of a phenolic-nylon ablator are presented. The analysis includes flow field coupling with the ablator surface, equilibrium chemistry, a step-function diffusion model and a coupled line and continuum radiation calculation. This report serves as the documentation, i e. users manual and operating instructions for the computer programs listed in the report.
Document ID
19730015582
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Engel, C. D. (Louisiana State Univ. Baton Rouge, LA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-112306
Report Number: NASA-CR-112306
Accession Number
73N24309
Funding Number(s)
CONTRACT_GRANT: NGR-19-001-059
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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