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高超声速飞行器气动热耗散、输运及转换技术研究进展 被引量:7
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作者 苟建军 肖爽 +2 位作者 胡嘉欣 高戈 龚春林 《宇航学报》 EI CAS CSCD 北大核心 2022年第8期983-999,共17页
针对高超声速飞行器面临的严重气动热集中、累积和时变问题,从气动热耗散、输运和转换三个方面,分别论述了被动热耗散材料、结构和主动热耗散技术,基于高导热材料、热管和工质对流的热输运技术,以及再生转换和热电转换技术的研究现状及... 针对高超声速飞行器面临的严重气动热集中、累积和时变问题,从气动热耗散、输运和转换三个方面,分别论述了被动热耗散材料、结构和主动热耗散技术,基于高导热材料、热管和工质对流的热输运技术,以及再生转换和热电转换技术的研究现状及其在高超声速飞行器上的应用案例,提出了上述技术在面临高超声速气动热时存在的问题。最后,针对高超声速飞行器气动热耗散、输运和转换技术的发展趋势进行了展望。 展开更多
关键词 高超声速飞行器 气动热管理 耗散 输运 转换
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Design and parametric optimization of thermal management of lithium-ion battery module with reciprocating air-flow 被引量:3
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作者 刘燕平 欧阳陈志 +1 位作者 江清柏 梁波 《Journal of Central South University》 SCIE EI CAS CSCD 2015年第10期3970-3976,共7页
Single cell temperature difference of lithium-ion battery(LIB) module will significantly affect the safety and cycle life of the battery. The reciprocating air-flow module created by a periodic reversal of the air flo... Single cell temperature difference of lithium-ion battery(LIB) module will significantly affect the safety and cycle life of the battery. The reciprocating air-flow module created by a periodic reversal of the air flow was investigated in an effort to mitigate the inherent temperature gradient problem of the conventional battery system with a unidirectional coolant flow with computational fluid dynamics(CFD). Orthogonal experiment and optimization design method based on computational fluid dynamics virtual experiments were developed. A set of optimized design factors for the cooling of reciprocating air flow of LIB thermal management was determined. The simulation experiments show that the reciprocating flow can achieve good heat dissipation, reduce the temperature difference, improve the temperature homogeneity and effectively lower the maximal temperature of the modular battery. The reciprocating flow improves the safety, long-term performance and life span of LIB. 展开更多
关键词 lithium-ion battery thermal management reciprocating air-flow temperature difference orthogonal optimization SIMULATION
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