A Combined Experimental and Computational Study of the LAPCAT II Supersonic Combustor-Reference-Cited by-同舟云学术

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A Combined Experimental and Computational Study of the LAPCAT II Supersonic Combustor

Published:2018-09-15 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference
language:
Short-container-title:

Author:

Vincent-Randonnier Axel¹,Sabelnikov Vladimir¹,Ristori A¹,Zettervall Niklas²,Fureby Christer²

Affiliation:

1. ONERA

2. Swedish Defense Research Agency (FOI)

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-5208

Reference65 articles.

1. Conceptual Study of a Combined-Cycle Engine for an Aerospace Plane

2. AIAA Education Series.;Heiser W.H

3. Demonstration of mode transition in a scramjet combustor

4. Tests of the JAPHAR dual mode ramjet engine

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1. Dual‐Mode Combustion Scramjet;Scramjet Propulsion;2022-11-18

2. Scramjet Combustor;Scramjet Propulsion;2022-11-18

3. Analysis, Computational Modeling, and Simulation;Scramjet Propulsion;2022-11-18

4. Penetration of a kerosene liquid jet injected in a high temperature Mach 2 supersonic crossflow;Experiments in Fluids;2022-09-20

5. Investigation of influence of detailed chemical kinetics mechanisms for hydrogen on supersonic combustion using large eddy simulation;International Journal of Hydrogen Energy;2019-02

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