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余西龙 [1]
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Date Issued：2021
Community：高温气体动力学国家重点实验室
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一种固液火箭发动机燃烧性能评估方法及系统
专利
发明专利. 一种固液火箭发动机燃烧性能评估方法及系统, 专利号: ZL202110081561.9, 申请日期: 2021-01-21, 授权日期: 2021-12-07
Inventors:
林鑫
;
张泽林
;
王泽众
;
李飞
;
余西龙
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View/Download：182/38
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Submit date：2022/01/14
RBCC发动机引射模态流态分析及性能研究
学位论文
博士论文，北京: 中国科学院大学, 2021
Authors:
陈 科挺
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View/Download：505/11
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Submit date：2022/01/11
RBCC
引射模态
流动形态
流动匹配
简化建模
斜爆轰发动机的推力性能理论分析
期刊论文
力学学报, 2021, 卷号: 53, 期号: 10, 页码: 2853-2864
Authors:
杨鹏飞
;
张子健
;
杨瑞鑫
;
滕宏辉
;
姜宗林
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View/Download：458/46
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Submit date：2022/03/16
斜爆轰波
发动机
推力性能
燃烧模式
