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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)
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High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH(马生虎);  Zhang QF(张启帆);  Zhang, Peng;  Zhang XY(张新宇)
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Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
Synthesis and characterization of light-weight porous ceramics used in the transpiration cooling 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 177, 页码: 438-445
Authors:  Zhang, Bo;  Huang, Jie;  Li, Weijie;  Huang, Haiming;  Zhao, Huanyu;  Peng JL(彭锦龙)
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Carbon fiber-reinforced silicon carbide porous ceramics  Permeability  Oxyacetylene flame test  Transpiration cooling  
Anomalous mechanical materials squeezing three-dimensional volume compressibility into one dimension 期刊论文
NATURE COMMUNICATIONS, 2020, 卷号: 11, 期号: 1, 页码: 7
Authors:  Jiang, Xingxing;  Molokeev, Maxim S;  Dong, Liyuan;  Dong, Zhichao;  Wang, Naizheng;  Kang, Lei;  Li, Xiaodong;  Li, Yanchun;  Tian, Chuan;  Peng SL(彭世镠);  Li, Wei;  Lin, Zheshuai
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Intelligent Force-Measurement System Use in Shock Tunnel 期刊论文
SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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artificial intelligence  BALANCE SYSTEM  deep learning  DESIGN  dynamic calibration  FLOWS  force-measurement system  strain-gauge balance  
Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Shock tunnel  High enthalpy  Aerodynamic force measurement  Strain gauge balance  
A Fast-Response Calorimeter with Dynamic Corrections for Transient Heat Transfer Measurements 期刊论文
APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 17, 页码: 22
Authors:  Zhang SZ(张仕忠);  Wang Q(汪球);  Li JP(李进平);  Zhang XY(张晓源);  Chen H(陈宏)
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calorimeter  shock tunnel  heat transfer measurement  hypersonic  
Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
Authors:  Xue R;  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
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Compressible boundary layer combustion  Skin-friction reduction  Boundary layer transition  Transition k-kl-w model  Hydrogen combustion  
Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
Authors:  Ma KF(马凯夫);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Scramjet engines  Shock-induced combustion ramjet engines  Supersonic combustion  Chapman-Jouguet detonation  
Experimental and numerical investigation on flow and heat transfer of impingement jet cooling of kerosene 期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2020, 卷号: 116, 页码: 8
Authors:  Du MM(杜蒙蒙);  Zhong FQ(仲峰泉);  Xing YF(邢云绯);  Zhang XY(张新宇)
Adobe PDF(2316Kb)  |  Favorite  |  View/Download：280/111  |  Submit date：2020/08/26
Impingement jets  Kerosene  Heat transfer coefficient  Pressure loss  Reynolds number