Aerodynamic Performance of Strut Injection for a Round Scramjet Combustor
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Publisher
American Institute of Aeronautics and Astronautics
Reference15 articles.
1. Tangential Injection from Overlaid Slots into a Supersonic Stream
2. Transverse Injection from Circular and Elliptic Nozzles into a Supersonic Crossflow
3. Normal, Sonic Helium Injection Through a Wedge-Shaped Orifice into Supersonic Flow
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1. Impact of cavity and ramp configuration on the combustion performance of a strut-based scramjet combustor;International Journal of Turbo & Jet-Engines;2023-08-24
2. Scramjet Combustor;Scramjet Propulsion;2022-11-18
3. Injection and mixing of single fuel jet in SCRAMJET engine;Scramjets;2020
4. Research progress on strut-equipped supersonic combustors for scramjet application;Progress in Aerospace Sciences;2018-11
5. Application of the vortex effects induced by the trailing wedge to enhance the mixing and combustion in the strut-based scramjet;Applied Thermal Engineering;2018-07
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