A Computational Study on Supersonic Combustion With Strut as Flame Holder
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Publisher
American Institute of Aeronautics and Astronautics
Reference5 articles.
1. Development of Hydrocarbon-Fueled Scramjet Engines: The Hypersonic Technology (HyTech) Program
2. Investigation of Kerosene Combustion Characteristics with Pilot Hydrogen in Model Supersonic Combustors
3. Ignition and Combustion Performance of Scramjet Combustors with Fuel Injection Struts
4. Numerical modeling of wall-injected scramjet experiments
5. Design and Analysis of Computer Experiments
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2. Introduction;Scramjet Combustion;2022
3. Numerical investigation on implications of four strut injectors on combustion characteristics of a Doubly-Dual cavity-based scramjet combustor;International Journal of Hydrogen Energy;2020-11
4. Research progress on strut-equipped supersonic combustors for scramjet application;Progress in Aerospace Sciences;2018-11
5. Effect of outflow vortex of 3D Inlet on fuel injection and mixing in a scramjet combustor;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02
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