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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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王晶 [14]
范学军 [14]
姚卫 [6]
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Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor
期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11
Authors:
Cheng D(程迪)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li L(李龙)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(2651Kb)
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Submit date:2019/09/09
Heat flux measurement
Kerosene
Supersonic combustion
Scramjet
Heat flux sensor
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3
期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Wu K(吴坤)
;
Fan XJ(范学军)
Adobe PDF(807Kb)
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Submit date:2018/07/17
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Wu K(吴坤)
;
Fan XJ(范学军)
Adobe PDF(805Kb)
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Submit date:2018/06/06
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Fan XJ(范学军)
;
Fan, Xuejun(xfan@imech.ac.cn)
Adobe PDF(1173Kb)
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Submit date:2018/01/16
Adiabatic Flame Temperature
Aerodynamics
Boundary Layer Flow
Boundary Layers
Chemical Analysis
Combustion
Computational Chemistry
Directed Graphs
Flow Separation
Mach Number
Principal Component Analysis
Regression Analysis
Sensitivity Analysis
Spacecraft
Supersonic Aerodynamics
Supersonic Aircraft
Transients
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor
会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
Authors:
Cheng D(程迪)
;
Wang J(王晶)
;
Gong J
;
Lu Y(陆阳)
;
Yao W(姚卫)
;
Li L(李龙)
;
Fan XJ(范学军)
;
Fan, Xuejun (xfan@imech.ac.cn)
Adobe PDF(2131Kb)
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Submit date:2017/05/05
Equivalence Ratios
Heat Flux Distributions
Heat Transfer Characteristics
Scramjet
Supercritical Kerosenes
Supersonic Combustion
Supersonic Combustors
Total Temperatures
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Yao W(姚卫)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li XP(李晓鹏)
;
Fan XJ(范学军)
Adobe PDF(1195Kb)
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Submit date:2016/07/01
Adiabatic Flame Temperature
Combustion
Directed Graphs
Flow Separation
Heat Flux
Kerosene
Large Eddy Simulation
Musculoskeletal System
Real Time Systems
Sensitivity Analysis
Spacecraft
Transients
Blowout Limits of Cavity-Stabilized Flame of Supercritical Kerosene in Supersonic Combustors
期刊论文
Journal of Propulsion and Power, 2014, 卷号: 30, 期号: 5, 页码: 1161-1166
Authors:
Zhang TC(张泰昌)
;
Wang J(王晶)
;
Qi L
;
Fan XJ(范学军)
;
Zhang P
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(442Kb)
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View/Download:746/248
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Submit date:2014/11/27
Blowout limits of supercritical kerosene in supersonic combustors
会议论文
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, United states, JUL 14-17, 2013
Authors:
Zhang TC(张泰昌)
;
Wang J(王晶)
;
Yuan YM(袁越明)
;
Li JG(李建国)
;
Yu G(俞刚)
;
Fan XJ(范学军)
;
Zhang TC(张泰昌)
Adobe PDF(619Kb)
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Submit date:2014/02/24
Development of integrated high temperature sensor for simultaneous measurement of wall heat flux and temperature
期刊论文
REVIEW OF SCIENTIFIC INSTRUMENTS, 2012, 卷号: 83, 期号: 7, 页码: 074901
Authors:
Li L(李龙)
;
Wang J(王晶)
;
Fan XJ(范学军)
;
Fan, XJ
;
Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(2757Kb)
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View/Download:1224/334
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Submit date:2013/01/18
Radiative Calibration
Facilities
Cavity
Gauge
Meter
Nist
Characteristics of compressible flow of supercritical kerosene
期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 1, 页码: 8-13
Authors:
Zhong FQ(仲峰泉)
;
Fan XJ(范学军)
;
Wang J(王晶)
;
Yu G(俞刚)
;
Li JG(李建国)
;
Fan, XJ
;
Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(484Kb)
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Submit date:2013/01/18
Supercritical Kerosene
Compressible Flow
Laval Nozzle
Isentropic Process
Aviation Kerosene
Combustion
Propulsion