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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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李进平 [16]
俞鸿儒 [13]
姜宗林 [9]
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马赫数10超燃冲压发动机燃烧室流动与传热变化特性分析
期刊论文
推进技术, 2023, 卷号: 44, 期号: 10, 页码: 117-125
Authors:
徐雪睿
;
仲峰泉
;
岳连捷
;
张旭
;
张晓源
;
张仕忠
;
李进平
Adobe PDF(2542Kb)
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Submit date:2023/10/26
超燃冲压发动机
理论模型
构型参数
燃烧室性能
壁面传热
On theory and methods for advanced detonation-driven hypervelocity shock tunnels
期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:
Jiang ZL(姜宗林)
;
Li JP(李进平)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Yu HR(俞鸿儒)
Adobe PDF(1090Kb)
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities
用于爆轰驱动的射流起爆实验研究
期刊论文
爆炸与冲击, 2019, 卷号: 39, 期号: 06, 页码: 13-22
Authors:
陆星宇
;
李进平
;
陈宏
;
俞鸿儒
Adobe PDF(1287Kb)
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Submit date:2019/09/12
爆轰
湍流射流
起爆
激波风洞
爆轰驱动
爆轰驱动高能起爆技术实验研究
期刊论文
中国科学. 技术科学, 2018, 卷号: 49, 期号: 03, 页码: 311-319
Authors:
陆星宇
;
李进平
;
陈宏
;
俞鸿儒
Unknown(1871Kb)
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Submit date:2019/05/09
高超声速
爆轰
起爆
激波风洞
高超声速条件下溢流液膜厚度测量方法
期刊论文
中国科学. 技术科学, 2018, 卷号: 48, 期号: 6, 页码: 629-638
Authors:
苑朝凯
;
李进平
;
陈宏
;
姜宗林
;
俞鸿儒
Adobe PDF(4824Kb)
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Submit date:2018/10/24
高超声速热防护
主动冷却
液膜厚度
电导法
一种新型瞬态量热计的研制
期刊论文
中国科学. 技术科学, 2018, 卷号: 48, 期号: 5, 页码: 558-564
Authors:
张仕忠
;
李进平
;
张晓源
;
陈宏
;
俞鸿儒
Adobe PDF(1892Kb)
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Submit date:2018/10/24
气动热测量
瞬态量热计
热流传感器
CVD金刚石片
激波风洞
高超声速飞行复现风洞理论与方法
期刊论文
力学学报, 2018, 卷号: 50, 期号: 6, 页码: 1283-1291
Authors:
姜宗林
;
李进平
;
胡宗民
;
刘云峰
;
俞鸿儒
Adobe PDF(634Kb)
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Submit date:2019/01/09
高超声速
激波风洞
复现飞行条件
爆轰驱动
缝合条件
高超声速溢流冷却实验研究
期刊论文
力学学报, 2018, 卷号: 50, 期号: 1, 页码: 1-8
Authors:
苑朝凯
;
李进平
;
陈宏
;
姜宗林
;
俞鸿儒
Adobe PDF(570Kb)
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Submit date:2018/10/24
高超声速热防护
主动冷却
溢流冷却
液膜
Shock relations in gases of heterogeneous thermodynamic properties
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
Authors:
Hu ZM(胡宗民)
;
Zhou K(周凯)
;
Peng J(彭俊)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
;
Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1654Kb)
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Submit date:2017/10/25
Shock Wave
Imperfect Gas
Heterogeneous
Theoretical Solution
Comparative study on aerodynamic heating under perfect and nonequilibrium hypersonic flows
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 2, 页码: 624701
Authors:
Wang Q(汪球)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
;
Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(763Kb)
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Submit date:2016/03/21
Aerodynamic Heating
Hypersonic
Shock Tunnel
Stanton Number
Sharp Cone