Experimental Investigations of Scramjet Combustor Characteristics-Reference-Cited by-同舟云学术

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Experimental Investigations of Scramjet Combustor Characteristics

Published:2008-04-28 Issue: Volume: Page:
ISSN:
Container-title:15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Scheuermann Tobias¹,Chun Jaechul¹,von Wolfersdorf Jens¹

Affiliation:

1. Institute of Aerospace Thermodynamics

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2552

Reference23 articles.

1. Comparison of Scramjet Engine Performance in Mach 6 Vitiated and Storage-Heated Air

2. Progress in Astronautics and Aeronautics;Schetz J. A.,1980

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1. Experimental study on combustion characteristics of supersonic combustor based on alternating-wedge strut;Chinese Journal of Aeronautics;2024-05

2. Suitability of helium gas as surrogate fuel for hydrogen in H2-Air non-reactive supersonic mixing studies;International Journal of Hydrogen Energy;2022-02

3. Quasi-one-dimensional Scramjet Combustor Flow Solver Using the Numerical Propulsion System Simulation;2018 Joint Propulsion Conference;2018-07-08

4. Uncertainty quantification of a generic scramjet engine using a probabilistic collocation and a hybrid approach;CEAS Aeronautical Journal;2018-05-29

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