Suitability of the k-ω turbulence model for scramjet flowfield simulations-Reference-Cited by-同舟云学术

Suitability of the k-ω turbulence model for scramjet flowfield simulations

Published:2011-10-07 Issue:4 Volume:70 Page:493-514
ISSN:0271-2091
Container-title:International Journal for Numerical Methods in Fluids
language:en
Short-container-title:Int. J. Numer. Meth. Fluids

Author:

Chan W.Y.K.¹,Jacobs P.A.²,Mee D.J.¹

Affiliation:

1. Centre for Hypersonics, School of Mechanical & Mining Engineering; The University of Queensland; Brisbane; Qld 4072; Australia

2. Queensland Geothermal Energy Centre of Excellence; School of Mechanical & Mining Engineering; The University of Queensland; Brisbane; Qld 4072; Australia

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference52 articles.

1. A century of ramjet propulsion technology evolution;Fry;Journal of Propulsion and Power,2004

2. Experimentation, test, and evaluation requirements for future airbreathing hypersonic systems;Marren;Journal of Propulsion and Power,2001

3. Advanced computational-fluid-dynamics techniques for scramjet combustion simulation;Ladeinde;AIAA Journal,2010

4. Reassessment of the scale-determining equation for advanced turbulence models;Wilcox;AIAA Journal,1988

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