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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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Study on aerodynamic loads at the inlet's cowl lip induced by multiple shock-shock interferences
期刊论文
ACTA MECHANICA SINICA, 2024, 卷号: 40, 期号: 4, 页码: 12
Authors:
Lin MY(林明月)
;
Yang F(杨帆)
;
Hu ZM(胡宗民)
;
Han GL(韩桂来)
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View/Download:18/0
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Submit date:2024/05/27
Shock waves
Shock-shock interaction
Theoretical analysis
Hysteresis
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:
Dai, Chunliang
;
Sun, Bo
;
Yue LJ(岳连捷)
;
Zhou, Shengbing
;
Zhuo, Changfei
;
Zhou, Changsheng
;
Yu, Jianyi
Adobe PDF(5674Kb)
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Submit date:2024/02/19
Scramjet inlet
Starting ability
Thermochemical
Work performance
Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474
Authors:
Yuan CK(苑朝凯)
;
Meng FZ(孟凡钊)
;
Liu, Xu
;
Liu YF(刘云峰)
;
Lian H(连欢)
;
Liu, Yingzheng
;
Peng, Di
Adobe PDF(3477Kb)
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Submit date:2023/07/17
Temperature-sensitive paint
Heat flux
Conjugate gradient method
Air-breathing hypersonic vehicle
Inverse heat conduction problem
高速弹丸诱导斜爆轰激波结构实验研究
期刊论文
力学学报, 2023, 卷号: 55, 期号: 02, 页码: 309-317
Authors:
尚甲豪
;
胡国暾
;
汪球
;
王业军
;
张坤
;
项高翔
;
赵伟
;
魏炳忱
Adobe PDF(1612Kb)
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Submit date:2023/03/16
斜爆轰
超声速燃烧
激波诱导燃烧
斜爆轰波
二级轻气炮
氨燃料吸气式变循环发动机性能分析
期刊论文
力学学报, 2022, 卷号: 54, 页码: 16
Authors:
张鑫
;
陆阳
;
程迪
;
范学军
Adobe PDF(1309Kb)
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Submit date:2022/10/17
氨
涡轮模态
预冷模态
冲压模态
当量总热沉
当量热值
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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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
高超声速高焓条件下的内嵌式温敏漆测量方法
期刊论文
力学学报, 2022, 卷号: 54, 期号: 01, 页码: 48-58
Authors:
苑朝凯
;
姜宗林
Adobe PDF(1381Kb)
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Submit date:2022/03/16
温敏漆
热流密度场
辐射效应
高超声速流动
辨识方法
沟槽微结构尺寸对高速列车横风特性影响研究
期刊论文
空气动力学学报, 2021, 卷号: 39, 期号: 05, 页码: 132-141
Authors:
王业腾
;
孙振旭
;
鞠胜军
;
王梦莹
;
杨国伟
Adobe PDF(1811Kb)
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Submit date:2022/03/16
高速列车
横风
表面微结构
气动性能
正交设计
方差分析
极差分析
Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
Adobe PDF(1806Kb)
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:
Jiang ZL(姜宗林)
;
Hu ZM(胡宗民)
;
Wang YP(汪运鹏)
;
Han GL(韩桂来)
Adobe PDF(1129Kb)
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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique