Search NASAโŒ• Search

NASA NTRS ยท 19930002821

Examination of various turbulence models for application in liquid rocket thrust chambers

Abstract

There is a large variety of turbulence models available. These models include direct numerical simulation, large eddy simulation, Reynolds stress/flux model, zero equation model, one equation model, two equation k-epsilon model, multiple-scale model, etc. Each turbulence model contains different physical assumptions and requirements. The natures of turbulence are randomness, irregularity, diffusivity and dissipation. The capabilities of the turbulence models, including physical strength, weakness, limitations, as well as numerical and computational considerations, are reviewed. Recommendations are made for the potential application of a turbulence model in thrust chamber and performance prediction programs. The full Reynolds stress model is recommended. In a workshop, specifically called for the assessment of turbulence models for applications in liquid rocket thrust chambers, most of the experts present were also in favor of the recommendation of the Reynolds stress model.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Hung, R. J.. 1991-04-30. Examination of various turbulence models for application in liquid rocket thrust chambers. https://ntrs.nasa.gov/citations/19930002821

Cite the original work for its findings. Save a collection to share your selection of sources.