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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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张新宇 [3]
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Indexed By:CSCD
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Author:张新宇
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Community:高温气体动力学国家重点实验室
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Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel
期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:
Xing YF(邢云绯)
;
Zhong FQ(仲峰泉)
;
Li DX(李东霞)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:475/208
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Submit date:2015/04/28
Hypersonic Scramjet Test Tunnel
Nozzle
Aerodynamic Heating
Convective Heat Transfer
The vitiation effects of water vapor and carbon dioxide on the autoignition characteristics of kerosene
期刊论文
Acta Mechanica Sinica, 2014, 卷号: 30, 期号: 4, 页码: 485-494
Authors:
Liang JH(梁金虎)
;
Wang S(王苏)
;
Zhang ST(张胜涛)
;
Yue LJ(岳连捷)
;
Fan BC(范秉诚)
;
Zhang XY(张新宇)
;
Cui JP(崔季平)
;
Wang S(王苏)
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Submit date:2014/08/14
Ignition Delay
Vitiation Effect
Kerosene
Water
Carbon Dioxide
Shock Tube
Measurements of non-equilibrium and equilibrium temperature behind a strong shock wave in simulated martian atmosphere
期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 5, 页码: 1296-1302
Authors:
Lin X
;
Yu XL(余西龙)
;
Li F(李飞)
;
Zhang SH(张少华)
;
Xin JG
;
Zhang XY(张新宇)
;
Yu, XL
;
Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2013/01/18
Radiation Measurements
Shock Wave
Mars Re-entry
Rotational Temperature
Vibrational Temperature
Radiation Measurements
Cn
Entry
Tube
Mixtures
Model