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Assessment of RANS and DES Turbulence Models for Supersonic Jet Interaction Flows

  • Published:2005-01-10 Issue: Volume: Page:
  • ISSN:
  • Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Srinivasan Ravichandra1,Bowersox Rodney1

Affiliation:

1. Texas A&M University

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. Prospects for future hypersonic air-breathing vehicles

2. Hypersonic Airbreathing Propulsion

3. 3Weber, R. and McKay, J. “Analysis of Ramjet Engines using Supersonic Combustion,” Tech. Rep. TN-4386, NACA, 1958.

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1. Computational Analysis of Transverse Sonic Injection in Supersonic Crossflow Using RANS Models;Journal of Fluids Engineering;2020-02-25

2. Interaction of Vortex with Bow Shock Wave: Computational Model, Experimental Validation, Enhanced Mixing;AIAA Journal;2018-08

3. Numerical and experimental investigation of transverse injection flows;Shock Waves;2010-02-24

4. Detached Eddy Simulation of a Generic Scramjet Inlet and Combustor;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

5. Hybrid RANS/LES of a Supersonic Combustor;26th AIAA Applied Aerodynamics Conference;2008-06-14
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