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A survey on numerical simulations of drag and heat reduction mechanism in supersonic/hypersonic flows 被引量:13
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作者 xiwan sun Wei HUANG +2 位作者 Min OU Ruirui ZHANG Shibin LI 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2019年第4期771-784,共14页
Along with the survey on experimental investigations drawing attention to the drag and heat reduction mechanism, the authors simultaneously focus on the recent advances of numerical simulations on the schemes applied ... Along with the survey on experimental investigations drawing attention to the drag and heat reduction mechanism, the authors simultaneously focus on the recent advances of numerical simulations on the schemes applied to supersonic/hypersonic vehicles. The CFD study has evolved as an irreplaceable method in scheme evaluation and aircraft optimization. Similar to our previous experimental survey, the advances in drag and heat reduction schemes are reviewed by similar kinds of mechanism in this article, namely the forward-facing cavity, the opposing jet, the aerospike, the energy deposition and their combinational configurations. This review article puts an emphatic eye on the flow conditions, numerical methods, novel schemes and analytical conclusions given in the simulations. Further, the multi-objective design optimization concept has also been illustrated due to the observable advantages of using CFD over experimental method, especially those performances conducted in drag reduction and thermal protection practice, and this would possess reference value in the design of aircraft system. 展开更多
关键词 Aerospike Drag and HEAT reduction Energy deposition Forward-facing CAVITY Opposing JET
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