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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... [13]
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范学军 [13]
姚卫 [6]
张泰昌 [5]
李晓鹏 [4]
王晶 [4]
陆阳 [4]
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2015 [13]
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第八届全国高超声速科... [4]
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Author:范学军
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Date Issued:2015
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Study on Flame Stabilization in a Dual-Mode Combustor Using Optical Measurements
期刊论文
JOURNAL OF PROPULSION AND POWER, 2015, 卷号: 31, 期号: 6, 页码: 1524-1531
Authors:
Yuan YM(袁越明)
;
Zhang TC(张泰昌)
;
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, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2016/03/21
一种拓展超声速燃烧火焰稳定极限的方法
专利
发明专利. 一种拓展超声速燃烧火焰稳定极限的方法, 专利号: ZL201310410973.8, 申请日期: 2013-09-11, 授权日期: 2015-10-14
Inventors:
张泰昌
;
王晶
;
范学军
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Submit date:2015/10/20
一种主动冷却亚燃冲压发动机燃油切换的系统和方法
专利
发明专利. 一种主动冷却亚燃冲压发动机燃油切换的系统和方法, 专利号: ZL201310451746.X, 申请日期: 2013-09-27, 授权日期: 2015-09-27
Inventors:
袁涛
;
陆阳
;
李龙
;
王晶
;
孟令瑾
;
范学军
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Submit date:2015/09/21
一种主动冷却亚燃冲压发动机冷却和燃烧闭环切换装置
专利
发明专利. 一种主动冷却亚燃冲压发动机冷却和燃烧闭环切换装置, 专利号: ZL201510452002.X, 申请日期: 2013-09-27, 授权日期: 2015-09-09
Inventors:
袁涛
;
李龙
;
陆阳
;
孟令瑾
;
黄鹏
;
范学军
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Submit date:2015/09/21
一种以加热煤油为燃料的超声速燃烧室
专利
发明专利. 一种以加热煤油为燃料的超声速燃烧室, 专利号: ZL201310411204.X, 申请日期: 2013-09-11, 授权日期: 2015-07-08
Inventors:
张泰昌
;
王晶
;
范学军
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Submit date:2015/07/10
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 comparative study of highly underexpanded nitrogen and hydrogenjets using large eddy simulation
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:
Li XP(李晓鹏)
;
Wu K(吴坤)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2017/05/05
Comparative Studies
Flow Charac
Teristics
High Order Harmonics
High Resolution
Instability Modes
Near
Field Structure
Shock Structure
Under
Expanded Jets
Three-dimensional numerical study of the acoustic properities of a highly underexpanded jet
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:
Wu K(吴坤)
;
Li XP(李晓鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(590Kb)
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View/Download:356/88
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Submit date:2017/05/05
Frequency Spectrum Analysis
High Temporal Resolution
Instantaneous Flow
Noise Generation Mechanisms
Theoretical Modeling
Three
Dimensional Numerical Studies
Transport Mechanism
Under
Expanded Jets
超声速燃烧熄火极限实验研究
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:
张泰昌
;
袁越明
;
范学军
;
张鹏
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Adobe PDF(625Kb)
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View/Download:346/70
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Submit date:2016/08/16
熄火极限
超声速燃烧
凹腔
火焰稳定
层流火焰
化学发光
剪切层
隔离段
速度计算
总温