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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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State Key... [12]
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范学军 [12]
陆阳 [12]
姚卫 [4]
李龙 [4]
王晶 [3]
程迪 [3]
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Creator:陆阳
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Document Type:会议论文
Author:范学军
Community:高温气体动力学国家重点实验室
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高动压超声速燃烧热防护初步分析
会议论文
空天飞行高温气动全国重点实验室(筹)2023年度夏季学术交流会暨高温气动学术前沿专题研讨会, 怀来, 2023-8-27 ~ 2023-8-29
Authors:
程迪
;
陆阳
;
范学军
Adobe PDF(1106Kb)
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View/Download:105/20
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Submit date:2023/11/30
超声速燃烧
高动压
热防护
一种逆流式空气预冷器的设计计算方法
会议论文
第六届空天动力联合会议暨中国航天第三专业信息网第四十二届技术交流会, 中国江苏苏州, 2022-11-23
Authors:
陈志霄
;
陆阳
;
邓清
;
范学军
Adobe PDF(1846Kb)
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Submit date:2023/04/14
空气预冷器
翅片
逆流
碳氢燃料
A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels
会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
Authors:
Jin YC(靳一超)
;
Wu K(吴坤)
;
Lu Y(陆阳)
;
Fan XJ(范学军)
Adobe PDF(1121Kb)
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Submit date:2022/07/04
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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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)
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View/Download:334/87
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Submit date:2018/12/26
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.
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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)
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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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Submit date:2016/01/08
Hydrocarbons
Combustors
Cooling
Heat Transfer
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
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)
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Submit date:2013/02/28