Hybrid Large Eddy Simulation/Reynolds-Averaged Navier–Stokes Analysis of a Premixed Ethylene-Fueled Dual-Mode Scramjet Combustor-Reference-Cited by-同舟云学术

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Hybrid Large Eddy Simulation/Reynolds-Averaged Navier–Stokes Analysis of a Premixed Ethylene-Fueled Dual-Mode Scramjet Combustor

Published:2021-07 Issue:7 Volume:59 Page:2440-2456
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Nielsen Tanner B.¹,Edwards Jack R.²,Chelliah Harsha K.³,Lieber Damien³,Geipel Clayton³,Goyne Christopher P.³,Rockwell Robert D.³,Cutler Andrew D.⁴

Affiliation:

1. Los Alamos National Laboratory, Los Alamos, New Mexico 87545

2. North Carolina State University, Raleigh, North Carolina 27695

3. University of Virginia, Charlottesville, Virginia 22904

4. The George Washington University, Newport News, Virginia 23602

Funder

Department of Defense

AFOSR

National Science Foundation

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J059343

Reference38 articles.

1. Development of a Premixed Combustion Capability for Dual-Mode Scramjet Experiments

2. From ignition to stable combustion in a cavity flameholder studied via 3D tomographic chemiluminescence at 20 kHz

3. Raman scattering measurements of mixing and finite-rate chemistry in a supersonic reacting flow over a piloted, ramped cavity

4. Large Eddy Simulation of High-Speed, Premixed Ethylene Combustion (Invited)

Cited by 11 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Design and analysis of an ideal scramjet flowpath;Physics of Fluids;2024-03-01

2. High-Fidelity Numerical Simulations of a Scramjet Flowpath;AIAA SCITECH 2024 Forum;2024-01-04

3. Experimental Study on Combustion Modes and Oscillations in a Cavity-Based Scramjet Combustor;AIAA Journal;2023-12-09

4. Experimental investigations of combustion oscillation modes in a large-aspect-ratio dual-mode combustor equipped with multi-strut;Physics of Fluids;2023-10-01

5. Mixing enhancement of ethylene secondary jet injected into supersonic cross-flow using curved pylon;Acta Astronautica;2023-09

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