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A New Method of Thermal Protection by Opposing Jet for a Hypersonic Aeroheating Strut 被引量:4
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作者 QIN Jiang NING Dongpo +3 位作者 FENG Yu ZHANG Junlong FENG Shuo BAO Wen 《Journal of Thermal Science》 SCIE EI CAS CSCD 2017年第3期282-288,共7页
This paper presents the numerical investigation of thermal protection of scramjet strut by opposing jet in supersonic stream of Mach number 6 with a hydrogen fueled scramjet strut model using CFD software. Simulation ... This paper presents the numerical investigation of thermal protection of scramjet strut by opposing jet in supersonic stream of Mach number 6 with a hydrogen fueled scramjet strut model using CFD software. Simulation results indicate that when a small amount of fuel is injected from the nose of the strut, the bow shock is pushed away from the strut, and the heat flux is reduced in the strut, especially at the leading edge. Opposing jet forms a recirculation region near the nozzle so that the strut is covered with low temperature fuel and separated from free stream. An appropriate total pressure ratio can be used to reduce not only aerodynamic heating but also the drag of strut. It is therefore concluded that thermal protection of scramjet strut by opposing jet is one of the promising ways to protect scramjet strut in high enthalpy stream. 展开更多
关键词 热保护 超音速冲压式喷气发动机神气 反对喷气
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