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NASA NTRS ยท 19950017224

Progress in Advanced Spray Combustion Code Integration

Abstract

A multiyear project to assemble a robust, muitiphase spray combustion code is now underway and gradually building up to full speed. The overall effort involves several university and government research teams as well as Rocketdyne. The first part of this paper will give an overview of the respective roles of the different participants involved, the master strategy, the evolutionary milestones, and an assessment of the state-of-the-art of various key components. The second half of this paper will highlight the progress made to date in extending the baseline Navier-Stokes solver to handle multiphase, multispecies, chemically reactive sub- to supersonic flows. The major hurdles to overcome in order to achieve significant speed ups are delineated and the approaches to overcoming them will be discussed.

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BibTeXRIS

Liang, Pak-Yan. 1993-07-01. Progress in Advanced Spray Combustion Code Integration. https://ntrs.nasa.gov/citations/19950017224

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