Large-Eddy/Reynolds-Averaged Navier–Stokes Simulations of Reactive Flow in Dual-Mode Scramjet Combustor-Reference-Cited by-同舟云学术

Large-Eddy/Reynolds-Averaged Navier–Stokes Simulations of Reactive Flow in Dual-Mode Scramjet Combustor

Published:2014-05 Issue:3 Volume:30 Page:558-575
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Fulton Jesse A.,Edwards Jack R.,Hassan Hassan A.,McDaniel James C.,Goyne Christopher P.,Rockwell Robert D.,Cutler Andrew D.¹,Johansen Craig T.²,Danehy Paul M.³

Affiliation:

1. Mechanical and Aerospace Engineering, George Washington University, Newport News, Virginia 23602

2. Mechanical and Manufacturing Engineering, University of Calgary, Calgary, Alberta T2N 1N4, Canada

3. Advanced Sensing and Optical Measurement Branch, NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34929

Reference38 articles.

1. BaurleR. A. “Modeling of High-Speed Reacting Flows: Established Practices and Future Challenges,” AIAA Paper 2004-0267, Jan. 2004.

2. GeninF.ChernyavskyB.MenonS. “Large Eddy Simulation of Scramjet Combustion Using a Subgrid Mixing/Combustion Model,” AIAA Paper 2003-7035, Dec. 2003.

3. Simulation of Turbulent Mixing Behind a Strut Injector in Supersonic Flow

4. LES of supersonic combustion in a scramjet engine model

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