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Theoretical study on the cooling procedure for vertical flow sinters
期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 127, 页码: 592-601
Authors:
Pan LS(潘利生)
;
Wei XL(魏小林)
;
Peng, Yan
;
Ma, Yuejing
;
Li B(李博)
;
Pan, LS (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2017/09/04
Vertical Flow Sinter Cooling Device
Sinter Layer
Convection Heat Transfer
Pressure Drop
Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 256-263
Authors:
Fang YS(方宜申)
;
Hu ZM(胡宗民)
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Ng HD
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Submit date:2018/02/08
Oblique Detonation
Equivalence Ratio
Mixture Inhomogeneity
Detailed Chemistry
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp
期刊论文
PHYSICS OF FLUIDS, 2017, 卷号: 29, 期号: 12, 页码: 125101
Authors:
Tong FL(童福林)
;
Li XL(李新亮)
;
Duan YH
;
Yu ZP(于长平)
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Submit date:2018/02/08
The dual information preserving method for stiff reacting flows
期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 157, 页码: 253-275
Authors:
Liu, Li
;
Shen YQ(申义庆)
;
Liu, Shengping
;
Yu, Ming
;
Shen, YQ (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Submit date:2017/11/16
Stiff Reacting Flow
Dual Information Preserving Method
Numerical Perturbation Method
Shock-capturing Scheme
Aerodynamic measurement of a large aircraft model in hypersonic flow
期刊论文
CHINESE PHYSICS B, 2017, 卷号: 26, 期号: 11, 页码: 114702-1-114702-6
Authors:
Meng BQ(孟宝清)
;
Han GL(韩桂来)
;
Zhang DL(张德良)
;
Jiang ZL(姜宗林)
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Submit date:2017/12/18
Hypersonic
Aerodynamic Measurement
Theoretical Study
Vibration
The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
Authors:
Li HX(李慧鑫)
;
Ye L(叶亮)
;
Wei XL(魏小林)
;
Li T(李腾)
;
Li S(李森)
;
Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2017/12/18
H2o2/kerosene Bipropellant
Coaxial-swirl Injector
Geometric Constant
Performance
超声速三维进气道内激波干扰的研究
期刊论文
推进技术, 2017, 期号: 12, 页码: 6
Authors:
项高翔
;
王春
;
汪运鹏
;
姜宗林
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Submit date:2017/12/22
高超声速流动
箱式进气道
侧壁压缩进气道
波系结构
流场区域
高温引气对亚燃冲压燃烧室性能影响的研究
期刊论文
推进技术, 2017, 期号: 12, 页码: 10
Authors:
王亚妹
;
方祥军
;
顾洪斌
;
林鹏
;
王霄
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Submit date:2017/12/22
亚燃冲压燃烧室
凹腔/支板结构
高温引气
混合效率
燃烧效率
分辨率优化的混合WENO格式
期刊论文
计算物理, 2017, 卷号: 35, 期号: 4, 页码: 397-404
Authors:
郭元
;
田奇
;
梁贤
;
李新亮
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Submit date:2018/10/24
混合格式
数值耗散
色散
保单调
优化
Flow characteristic of highly underexpanded jets from various nozzle geometries
期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
Authors:
Li XP(李晓鹏)
;
Zhou, Rui
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (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:2017/11/16
Underexpanded Jets
Noncircular Jets
Nozzle Geometry
Large Eddy Simulation