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负泊松比结构力学设计、抗冲击性能及在车辆工程应用与展望 期刊论文
力学学报, 2021, 卷号: 53, 期号: 03, 页码: 611-638
Authors:  吴文旺;  肖登宝;  孟嘉旭;  刘凯;  牛迎浩;  薛睿;  张鹏;  丁文杰;  叶璇;  凌雪;  毕颖;  夏勇
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负泊松比  拉胀  冲击吸能  车辆轻量化  
Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 卷号: 37, 期号: 3, 页码: 3685-3692
Authors:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军)
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Supersonic combustion  Flame stabilization mode  DLR Strut injection scheme  Stagnation Temperature  Overall equivalence ratio  
Modeling Analysis on Cavity-based Flame Stabilization in Scramjet Combustor 会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
Authors:  Wu K(吴坤);  Zhang P(张鹏);  Fan XJ(范学军)
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Combustion chemistry  Combustion dynamics  Dual  mode scramjet  Flame stabilization  Improved delayed detached eddy simulations  Overall reactions  Scramjet combustors  Shock  wave structures  
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
Authors:  Yue LJ(岳连捷);  Jia YN(贾轶南);  Xu X;  Zhang XY(张新宇);  Zhang P(张鹏)
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Inlet restart  Cowl shock  Shock wave boundary layer interactions  
Characterization of flame stabilization modes in an ethylene-fueled supersonic combustor using time-resolved CH* chemiluminescence 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 卷号: 36, 期号: 2, 页码: 2919-2925
Authors:  Yuan YM(袁越明);  Zhang TC(张泰昌);  Yao W(姚卫);  Fan XJ(范学军);  Zhang P(张鹏);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, PR, Peoples R China.
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Supersonic Combustion  Flame Stabilization  Stagtnation Temperature  Gloabal Equivalence Ratio  Ch** Ch*emiluminesenCh*e  
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, Peng(
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Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
Numerical Investigation on Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 卷号: 189, 期号: 12, 页码: 2154-2179
Authors:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, P (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong 999077, Hong Kong, Peoples R China.
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Detailed Hydrogen Oxidation Mechanism  Dlr  Flame Stabilization  Sensitivity Analysis  Supersonic Combustion  
超声速燃烧稳焰模式分布研究 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:  袁越明;  张泰昌;  范学军;  张鹏
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火焰结构  超声速燃烧  凹腔  当量比  燃烧室内  火焰稳定  总温  一维性  隔离段  参数空间  
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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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  
高Bond数下黏性液滴的Rayleigh-Taylor不稳定性 期刊论文
力学学报, 2006, 卷号: 38, 期号: 3, 页码: 289-295
Authors:  张鹏;  俞刚
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液滴  破碎  Rayleigh-taylor不稳定性  Bond数  黏性