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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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范学军 [8]
陆阳 [8]
姚卫 [4]
李龙 [4]
程迪 [3]
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Creator:范学军
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Creator:陆阳
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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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View/Download:416/136
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Submit date:2019/09/09
Heat flux measurement
Kerosene
Supersonic combustion
Scramjet
Heat flux sensor
A novel method of cooling channel optimization for active-cooled structure using the calculus of variations
会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:
Li X(李轩)
;
Lu Y(陆阳)
;
Wu K(吴坤)
;
Fan XJ(范学军)
Adobe PDF(705Kb)
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View/Download:183/63
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Submit date:2020/11/20
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network
会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
Authors:
Li B
;
Lee YC(李亚超)
;
Yao W(姚卫)
;
Lu Y(陆阳)
;
Fan XJ(范学军)
Adobe PDF(1813Kb)
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Submit date:2018/12/26
Development of a radiative heating facility for studying flow and heat transfer in hydrocarbon-cooled structures
期刊论文
REVIEW OF SCIENTIFIC INSTRUMENTS, 2018, 卷号: 89, 期号: 6, 页码: 64901
Authors:
Dong D(董达)
;
Lu Y(陆阳)
;
Yuan YM(袁越明)
;
Fan XJ(范学军)
Adobe PDF(4017Kb)
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Submit date:2018/10/30
Development of a radiative heating system for studies of heat transfer in fuel-cooled structures
会议论文
14th International Energy Conversion Engineering Conference, Salt Lake City, UT, JUL 25-27, 2016
Authors:
Dong D(董达)
;
Lu Y(陆阳)
;
Yuan YM(袁越明)
;
Fan XJ(范学军)
;
Dong, D (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(637Kb)
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Submit date:2017/05/12
Aviation Kerosene
Supercritical Conditions
Pressure
Rp-3
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
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
Authors:
Lu Y(陆阳)
;
Wang XZ(王新竹)
;
Li L(李龙)
;
Cheng D(程迪)
;
Yuan T(袁涛)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(445Kb)
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View/Download:457/94
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Submit date:2016/01/08
Hydrocarbons
Combustors
Cooling
Heat Transfer
A Thermal Analysis Method for Fuel-Cooled Combustor Structure based on Heat Flux Measurement
会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference., Tours,France, 2012.9.24-28
Authors:
Lu Y(陆阳)
;
Li L(李龙)
;
Fan XJ(范学军)
Adobe PDF(483Kb)
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Submit date:2013/02/28