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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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Heat Recuperation for the Self-Condensing CO
2
Transcritical Power Cycle
期刊论文
JOURNAL OF THERMAL SCIENCE, 2024, 页码: 12
Authors:
Pan LS(潘利生)
;
Shi, Weixiu
;
Sun, Yin
;
Sun, Yiwei
;
Wei XL(魏小林)
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View/Download:23/0
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Submit date:2024/05/21
CO2 transcritical power cycle
heat recuperation process
self-condensing
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
Experimental Investigation of the Operating Characteristics of a Pulsating Heat Pipe with Ultra-Pure Water and Micro Encapsulated Phase Change Material Suspension
期刊论文
JOURNAL OF THERMAL SCIENCE, 2023
Authors:
Shi, Weixiu
;
Su, Xiaoyang
;
Chen, Hongdi
;
Pan LS(潘利生)
Adobe PDF(2591Kb)
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Submit date:2023/07/17
pulsating heat pipe (PHP)
micro encapsulated phase change material (MEPCM)
heat transfer characteristic
inclination angle
An analytical model for maximum temperature and temperature distribution of plate structure with active cooling
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 5, 页码: 322290
Authors:
Hu GH(胡国豪)
;
Zhong FQ(仲峰泉)
;
Chen KT(陈科挺)
Adobe PDF(2013Kb)
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Submit date:2023/04/20
Plate structure
Active cooling
Thermal protection
Convective heat transfer
Analytical model
Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 96-106
Authors:
Peng J(彭俊)
;
Li S(李帅)
;
Yang F(杨帆)
;
Lin MY(林明月)
;
Han GL(韩桂来)
;
Hu ZM(胡宗民)
Adobe PDF(2838Kb)
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Submit date:2023/04/20
Shock interactions
Transitional configuration
Aerodynamic heating
Shear layer
Mach interaction
基于主动射流控制的高超声速进气道再起动性能研究(英文)
期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:
靳一超
;
姚卫
Adobe PDF(1844Kb)
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Submit date:2023/02/09
高超声速进气道
不起动
再起动
主动射流
流动控制
Oblique detonation wave triggered by a double wedge in hypersonic flow
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184
Authors:
Teng, Honghui
;
Zhang, Yuhang
;
Yang PF(杨鹏飞)
;
Jiang ZL(姜宗林)
Adobe PDF(1747Kb)
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Submit date:2022/07/18
Double wedge
Hypersonic flow
Initiation structures
Oblique detonation
Shock interactions
Theories and methods for designing hypersonic high-enthalpy flow nozzles
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(2554Kb)
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Submit date:2022/06/10
Boundary layer correction
High-enthalpy flow
Hypersonic wind tunnel
Nozzle design
Real-gas effects
Parameters for evaluating the efficiency of inlet compression
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:
Chen KT(陈科挺)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(511Kb)
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Submit date:2022/01/12
Airbreathing engine
Compression efficiency
Compression quality
Inlet
Self-consistency
Reconstructing shock front of unstable detonations based on multi-layer perceptron
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:
Zhou, Lin
;
Teng, Honghui
;
Ng, Hoi Dick
;
Yang PF(杨鹏飞)
;
Jiang ZL(姜宗林)
Adobe PDF(6382Kb)
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Submit date:2021/11/01
Cellular detonation
Lead shock evolution
Multi-layer perceptron
Numerical simulations