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Knowledge Management System of Institue of Mechanics, CAS
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Source Publication：推进技术
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飞行高度对固体火箭两相喷焰流动与辐射的影响
期刊论文
推进技术, 2021, 卷号: 42, 期号: 03, 页码: 569-577
Authors:
包醒东
;
余西龙
;
王振华
;
毛宏霞
;
肖志河
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Submit date：2021/04/19
固体火箭发动机
两相流
喷焰
飞行高度
流场特性
辐射特性
