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范学军 [34]
姚卫 [21]
吴坤 [11]
陆阳 [9]
李晓鹏 [7]
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基于变分法的冷却结构优化设计与分析方法
期刊论文
推进技术, 2020, 卷号: 41, 期号: 05, 页码: 1121-1129
Authors:
李轩
;
陆阳
;
吴坤
;
范学军
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Submit date:2020/07/15
变分
冷却
优化
自适应
多目标
Hypergolic ignition modulated by head-on collision, intermixing and convective cooling of binary droplets with varying sizes
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 卷号: 139, 页码: 475-481
Authors:
Zhang DW
;
Yu DH
;
Zhang P
;
Yuan YM(袁越明)
;
Yue LJ(岳连捷)
;
Zhang TC(张泰昌)
;
Fan XJ(范学军)
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Submit date:2019/09/09
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
Adobe PDF(6645Kb)
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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
Influences of Domain Symmetry on Supersonic Combustion Modeling
期刊论文
JOURNAL OF PROPULSION AND POWER, 2019, 卷号: 35, 期号: 2, 页码: 451-465
Authors:
Yao W(姚卫)
;
Wu K(吴坤)
;
Fan XJ(范学军)
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Submit date:2019/04/11
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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Submit date:2018/12/27
Supersonic combustion
Flame stabilization mode
DLR Strut injection scheme
Stagnation Temperature
Overall equivalence ratio
Influence of compressibility effect on supersonic combustion modeling
会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:
Chen L
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2020/11/20
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)
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Submit date:2020/11/20
Shock oscillation in highly underexpanded jets
期刊论文
CHINESE PHYSICS B, 2018, 卷号: 27, 期号: 9, 页码: 94705
Authors:
Li XP
;
Zhou R
;
Chen XP
;
Fan XJ(范学军)
;
Xie GS
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Submit date:2018/10/30
highly underexpanded jets
shock oscillation
large eddy simulation
Low-Dissipative Hybrid Compressible Solver Designed for Large-Eddy Simulation of Supersonic Turbulent Flows
期刊论文
AIAA JOURNAL, 2018, 卷号: 56, 期号: 8, 页码: 3086-3096
Authors:
Lee YC(李亚超)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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View/Download:417/126
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Submit date:2018/10/19
Modeling Analysis of an Actively Cooled Scramjet Combustor Under Different Kerosene/Air Ratios
期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 4, 页码: 975-991
Authors:
Yao W(姚卫)
;
Lu Y(陆阳)
;
Wu K(吴坤)
;
Wang J(王晶)
;
Fan XJ(范学军)
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Adobe PDF(2427Kb)
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View/Download:379/115
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Submit date:2018/10/19