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NASA NTRS · 19840004196

Aerothermal modeling program, phase 1

Abstract

Aerothermal submodels used in analytical combustor models are analyzed. The models described include turbulence and scalar transport, gaseous full combustion, spray evaporation/combustion, soot formation and oxidation, and radiation. The computational scheme is discussed in relation to boundary conditions and convergence criteria. Also presented is the data base for benchmark quality test cases and an analysis of simple flows.

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BibTeXRIS

Srinivasan, R., Reynolds, R., Ball, I., Berry, R., Johnson, K., Mongia, H.. 1983-08-01. Aerothermal modeling program, phase 1. https://ntrs.nasa.gov/citations/19840004196

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