IMECH-IR
(Note: the search results are based on claimed items)

Browse/Search Results:  1-10 of 14 Help

Filters                            
Selected(0)Clear Items/Page:    Sort:
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)
View  |  Adobe PDF(807Kb)  |  Favorite  |  View/Download:354/111  |  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)
View  |  Adobe PDF(805Kb)  |  Favorite  |  View/Download:408/153  |  Submit date:2018/06/06
Flow characteristic of highly underexpanded jets from various nozzle geometries 期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
Authors:  Li XP(李晓鹏);  Zhou, Rui;  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, Beijing 100190, Peoples R China.
View  |  Adobe PDF(5723Kb)  |  Favorite  |  View/Download:430/188  |  Submit date:2017/11/16
Underexpanded Jets  Noncircular Jets  Nozzle Geometry  Large Eddy Simulation  
高度欠膨胀声速射流的自相似特性 期刊论文
航空动力学报, 2017, 卷号: 32, 期号: 01, 页码: 177-187
Authors:  李晓鹏;  姚卫;  范学军
View  |  Adobe PDF(767Kb)  |  Favorite  |  View/Download:293/86  |  Submit date:2017/12/22
高度欠膨胀射流  大涡模拟  自相似特性  高斯拟合  剪切层发展  
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)
View  |  Adobe PDF(1173Kb)  |  Favorite  |  View/Download:462/225  |  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
View  |  Adobe PDF(1818Kb)  |  Favorite  |  View/Download:343/99  |  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  
不同喷压比下欠膨胀射流对特征频率激励的响应 会议论文
第九届全国流体力学学术会议, 中国江苏南京, 2016-10-20
Authors:  李晓鹏;  姚卫;  范学军
View  |  Adobe PDF(122Kb)  |  Favorite  |  View/Download:393/82  |  Submit date:2017/09/27
欠膨胀射流  喷压比  特征频率激励  大涡模拟  流动响应  
A comparative study of highly underexpanded nitrogen and hydrogen jets using large eddy simulation 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2016, 卷号: 41, 期号: 9, 页码: 5151-5161
Authors:  Li XP(李晓鹏);  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军);  Li, XP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(728Kb)  |  Favorite  |  View/Download:357/124  |  Submit date:2016/09/14
Scramjet  Hydrogen  Highly Underexpanded Jet  Large Eddy Simulation  
Large-Eddy Simulation of Time Evolution and Instability of Highly Underexpanded Sonic Jets 期刊论文
AIAA JOURNAL, 2016, 卷号: 54, 期号: 10, 页码: 3191-3211
Authors:  Li XP(李晓鹏);  Yao W(姚卫);  Fan XJ(范学军);  Li, XP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(2106Kb)  |  Favorite  |  View/Download:396/145  |  Submit date:2016/12/08
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)  |  Favorite  |  View/Download:486/176  |  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