Large eddy simulations of the HIFiRE scramjet using a compressible flamelet/progress variable approach-Reference-Cited by-同舟云学术

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Large eddy simulations of the HIFiRE scramjet using a compressible flamelet/progress variable approach

Published:2015 Issue:2 Volume:35 Page:2163-2172
ISSN:1540-7489
Container-title:Proceedings of the Combustion Institute
language:en
Short-container-title:Proceedings of the Combustion Institute

Author:

Saghafian Amirreza,Shunn Lee,Philips David A.,Ham Frank

Funder

Office of Science of the U.S. Department of Energy

Air Force Research Laboratory STTR program

Publisher

Elsevier BV

Subject

Physical and Theoretical Chemistry,Mechanical Engineering,General Chemical Engineering

Reference35 articles.

1. J.M. Tishkoff, J.P. Drummond, T. Edwards, A.S. Nejad, AIAA Paper 97-1017, 1997.

2. The challenge of turbulent combustion

3. Assumed and evolution probability density functions in supersonic turbulent combustion calculations

4. Evaluation of combustion models for high speed H2/air confined mixing layer using DNS data

5. Assumed PDF turbulence-chemistry closure with temperature-composition correlations

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