Dual Cavity Scramjet Operability and Performance Study
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Publisher
American Institute of Aeronautics and Astronautics
Reference11 articles.
1. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview
2. Effect of Flame-Holding Cavities on Supersonic-Combustion Performance
3. Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors
4. Mixing and Combustion Studies Using Cavity-Based Flameholders in a Supersonic Flow
5. Characteristics of Cavity-Stabilized Flames in a Supersonic Flow
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1. Numerical Analysis of Supersonic Flow Past a Double Cavity Scramjet Combustor;Lecture Notes in Mechanical Engineering;2024
2. Examining Distributed Fueling Schemes Using Tandem Cavities in a Mach 8 Scramjet;Journal of Spacecraft and Rockets;2023-10-26
3. Experimental Study on the Ignition Characteristics of Scramjet Combustor with Tandem Cavities Using Micro-Pulse Detonation Engine;Aerospace;2023-08-11
4. 超音速流における気流境界層吸込みが流れ場および保炎性能へ与える影響;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023
5. Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity;Acta Astronautica;2015-03
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