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Knowledge Management System of Institue of Mechanics, CAS
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李进平 [4]
于江鹏 [2]
岳连捷 [2]
张启帆 [2]
张旭 [2]
张晓源 [2]
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Creator:李进平
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Date Issued:2022
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高马赫数燃烧强化的激波风洞试验研究
期刊论文
力学学报, 2022, 卷号: 54, 期号: 05, 页码: 1403-1413
Authors:
张旭
;
张启帆
;
岳连捷
;
孟东东
;
罗苇航
;
于江鹏
;
张晓源
;
李进平
;
陈宏
;
李飞
Adobe PDF(3069Kb)
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View/Download:252/46
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Submit date:2022/08/11
高马赫数
超声速燃烧
燃烧强化
小支板
JF-24激波风洞
一种利用气体压力能制冷的试验装置及控制方法
专利
发明专利. 一种利用气体压力能制冷的试验装置及控制方法, 专利号: ZL202111003835.9, 申请日期: 2021-08-30, 授权日期: 2022-05-17
Inventors:
杨丛笑
;
汪球
;
赵伟
;
栗继伟
;
李进平
Adobe PDF(632Kb)
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View/Download:140/46
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Submit date:2022/10/14
Numerical and Experimental Study on the Duration of Nozzle Starting of the Reflected High-Enthalpy Shock Tunnel
期刊论文
APPLIED SCIENCES-BASEL, 2022, 卷号: 12, 期号: 6, 页码: 16
Authors:
Yu JP(于江鹏)
;
Li JP(李进平)
;
Wang Q(汪球)
;
Zhang XY(张晓源)
;
Zhang SZ(张仕忠)
Adobe PDF(6583Kb)
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View/Download:337/150
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Submit date:2022/05/17
nozzle starting
high-enthalpy shock tunnel
center startup
complete startup
高马赫数超燃冲压发动机技术研究进展
期刊论文
力学学报, 2022, 卷号: 54, 期号: 02, 页码: 263-288
Authors:
岳连捷
;
张旭
;
张启帆
;
陈科挺
;
李进平
;
陈昊
;
姚卫
;
仲峰泉
;
李飞
;
王春
;
陈宏
Adobe PDF(2622Kb)
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View/Download:557/103
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Submit date:2022/03/16
高马赫数
超燃冲压发动机
热化学非平衡
超声速燃烧
低雷诺数流动
激波风洞
飞行试验