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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 ... [6]
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李晓鹏 [6]
范学军 [6]
姚卫 [5]
王晶 [4]
吴坤 [3]
袁越明 [3]
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Creator:李晓鹏
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不同喷压比下欠膨胀射流对特征频率激励的响应
期刊论文
推进技术, 2019, 卷号: 40, 期号: 06, 页码: 1239-1246
Authors:
李晓鹏
;
周蕊
;
庄法坤
;
曹逻炜
;
谢国山
;
范学军
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View/Download:383/52
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Submit date:2019/09/12
欠膨胀射流
喷压比
特征频率激励
大涡模拟
流动响应
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)
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View/Download:356/112
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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)
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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)
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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
高度欠膨胀射流的瞬态近场结构
期刊论文
推进技术, 2016, 卷号: 37, 期号: 12, 页码: 2233-2242
Authors:
李晓鹏
;
吴坤
;
姚卫
;
范学军
Adobe PDF(1818Kb)
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Submit date:2017/12/26
高度欠膨胀射流
大涡模拟
近场结构
瞬态非定常特征
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