Experimental Study on Combustion Mode Transition in a Scramjet with Parallel Injection-Reference-Cited by-同舟云学术

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Experimental Study on Combustion Mode Transition in a Scramjet with Parallel Injection

Published:2006-06-15 Issue: Volume: Page:
ISSN:
Container-title:14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Chun Jaechul¹,Scheuermann Tobias¹,von Wolfersdorf Jens¹,Weigand Bernhard¹

Affiliation:

1. University of Stuttgart

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-8063

Reference22 articles.

1. Hyper-X: Foundation for future hypersonic launch vehicles

2. Preliminary X-43 flight test results

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

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1. Prospects for scramjet engines in reusable launch applications: A review;International Journal of Hydrogen Energy;2023-11

2. Numerical study on the dynamic process of ramjet/scramjet mode transition in the integrated full flow path for RBCC engine;Applied Thermal Engineering;2023-08

3. Non-Intrusive Velocimetry in a Supersonic Reacting Flow using Two-Point Focused Laser Differential Interferometry;AIAA SCITECH 2023 Forum;2023-01-19

4. Mode Transition in a Strut Based Dual-Mode Scramjet Combustor;AIAA AVIATION 2022 Forum;2022-06-20

5. Reduced Order Model Based on Gradient Optimization for Two Dimensional Scramjet Inlets;AIAA SCITECH 2022 Forum;2022-01-03

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