Numerical Simulation of Transient Scramjet Combustion in a Shock Tunnel-Reference-Cited by-同舟云学术

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Numerical Simulation of Transient Scramjet Combustion in a Shock Tunnel

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

Star Jason¹,Edwards Jack¹,Smart Michael²,Baurle Robert²

Affiliation:

1. North Carolina State University

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-428

Reference33 articles.

1. Heiser,W.H.,andPratt,D.T.,HypersonicAirbreathingPropulsion,AIAAEducationSeries,Washington,DC,1994.

2. Odam, J., and Paull, A. "Internal Combustor Scramjet Pressure Measurements in the T4 Shock Tunnel," AIAA Paper 2002-5244.

3. Scramjet measurements in a shock tunnel

4. Experiments on supersonic combustion ramjet propulsion in a shock tunnel

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1. Analysis of a Multi-Porthole Injector Array in a Supersonic Crossflow;Journal of Propulsion and Power;2020-07

2. Quasi-One-Dimensional and Two-Dimensional Numerical Simulation of Scramjet Combustors;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23

3. Unsteady Thermo-Gasdynamic Processes in Scramjet Combustion Chamber with Periodical Input of Cold Air;50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2014-07-25

4. Numerical Investigation of Dual-Mode Operation in a Rectangular Scramjet Flowpath;Journal of Propulsion and Power;2014-03

5. Numerical Simulation of Shock-Induced-Combustion in Three-Dimensional HyShot Scramjet Model;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

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