Hybrid Large-Eddy Simulation / Reynolds-Averaged Navier-Stokes Simulations of Sonic Injection into Mach 2 Crossflow-Reference-Cited by-同舟云学术

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Hybrid Large-Eddy Simulation / Reynolds-Averaged Navier-Stokes Simulations of Sonic Injection into Mach 2 Crossflow

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Boles John¹,Milligan Ryan¹,Hagenmaier Mark²,Edwards Jack³

Affiliation:

1. Taitech, Inc.

2. Air Force Research Laboratory

3. North Carolina State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-769

Reference15 articles.

1. Prediction of Transverse Injection of a Sonic Jet in Supersonic Crossflow

2. Large-Eddy/Reynolds-Averaged Navier-Stokes Simulations of Sonic Injection into Mach 2 Crossflow

3. A New Version of Detached-eddy Simulation, Resistant to Ambiguous Grid Densities

Cited by 5 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. Effect of Injection Mach Number on Penetration in a Supersonic Crossflow;AIAA Journal;2020-03

2. Mixing Characteristics of a Gaseous Jet in a Supersonic Crossflow;Jet in Supersonic Crossflow;2019

3. Large-Eddy Simulation/Reynolds-Averaged Navier–Stokes Simulations of High-Speed Mixing Processes;AIAA Journal;2014-07

4. Supersonic jet and crossflow interaction: Computational modeling;Progress in Aerospace Sciences;2013-02

5. Hybrid LES/RANS Simulations of Shock-Distorted Injection Plumes;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

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