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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 [42]
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Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:
Fan WH(范文慧)
;
Zhong FQ(仲峰泉)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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Submit date:2020/03/11
Wall heat flux
Numerical simulation
Ethylene
Supersonic combustor
航空煤油冲击射流强化传热的实验研究
会议论文
中国航天第三专业信息网第四十届技术交流会暨第四届空天动力联合会议, 中国云南昆明, 2019-08-14
Authors:
杜蒙蒙
;
仲峰泉
;
邢云绯
;
张新宇
Adobe PDF(987Kb)
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Submit date:2020/09/28
实验研究
冲击射流
航空煤油
强化传热
CH* Luminance Distribution Application and a One-Dimensional Model of the Supersonic Combustor Heat Release Quantization
期刊论文
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2019, 卷号: 36, 期号: 1, 页码: 45-50
Authors:
Wang ZP(王知溥)
;
Gu HB(顾洪斌)
;
Cheng L W
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
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Submit date:2019/04/11
supersonic combustion
one-dimensional modelling
heat release
CH* chemiluminescence
氢燃料超声速燃烧火焰辐射与传热特性的大涡模拟研究
会议论文
中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议, 中国陕西西安, 2016-08-17
Authors:
马素刚
;
仲峰泉
;
张新宇
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Submit date:2017/09/27
大涡模拟
火焰辐射
离散坐标法
超声速燃烧
氢燃料
Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor
期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
Authors:
Wang X
;
Zhong FQ(仲峰泉)
;
Gu HB(顾宏斌)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Supersonic Combustor
Convective Heat Transfer
Numerical Study
Wall Heat Flux
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate
期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
Authors:
Zhong FQ(仲峰泉)
;
Ma SG
;
Zhang XY(张新宇)
;
Sung CJ
;
Niemeyer KE
;
Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Reduced Chemistry
Hydrocarbons
Directed Relation Graph
Ignition Delay Time
H_2O/CO_2污染对RP-3航空煤油着火特性的影响
期刊论文
推进技术, 2015, 卷号: 36, 期号: 3, 页码: 336-344
Authors:
梁金虎
;
王苏
;
张灿
;
张胜涛
;
岳连捷
;
范秉诚
;
张新宇
;
崔季平
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Submit date:2015/12/25
污染效应
着火延时
煤油
H2o
Co2
激波管
Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Ma SG(马素刚)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Zhong, Fengquan (fzhong@imech.ac.cn)
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Submit date:2017/05/05
Combustion Pro
Cess
Directed Relation Graph
Dynamic Evolution
Fuel Injection Velocities
Kinetic Mechanism
Reduced Mechanisms
Temperature Profiles
Temporal And Spatial Evolutions
防热复合材料烧蚀过程数值模拟
会议论文
第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28
Authors:
唐立富
;
万田
;
张新宇
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Adobe PDF(677Kb)
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Submit date:2016/08/16
烧蚀率
热化学平衡
热解动力学
牛顿迭代法
材料层
查表法
数学模型
防热
过程数值模拟
能量方程
激励频率对射流混合层主导频率影响的实验研究
会议论文
第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28
Authors:
闫继东
;
顾洪斌
;
张新宇
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Submit date:2016/08/16
激励频率
主频区
混合层
几何参数
扩散程度
Hartman