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岳连捷 [12]
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Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:
Dai, Chunliang
;
Sun, Bo
;
Yue LJ(岳连捷)
;
Zhou, Shengbing
;
Zhuo, Changfei
;
Zhou, Changsheng
;
Yu, Jianyi
Adobe PDF(5674Kb)
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Submit date:2024/02/19
Scramjet inlet
Starting ability
Thermochemical
Work performance
激波风洞两级入轨飞行器纵向级间分离试验技术
期刊论文
航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126
Authors:
王粤
;
汪运鹏
;
姜宗林
Adobe PDF(6797Kb)
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View/Download:395/39
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Submit date:2022/12/01
两级入轨
轨迹捕获
激波风洞
多体分离
动态试验
试验技术
Decomposition of mean skin friction in incident shock wave/turbulent boundary layer interaction flows at Mach 2.25
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 9, 页码: 178-194
Authors:
Duan JY(段俊亦)
;
Tong FL(童福林)
;
Li XL(李新亮)
;
Liu HW(刘洪伟)
Adobe PDF(6039Kb)
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View/Download:121/8
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Submit date:2023/11/13
Compressible flow
Boundary layers
Direct numerical simulation
Shock waves
Skin friction
Turbulent flow
Hypersonic shock wave and turbulent boundary layer interaction in a sharp cone/flare model
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 80-95
Authors:
Tong FL(童福林)
;
Duan JY(段俊亦)
;
Lai, Jiang
;
Sun, Dong
;
Yuan, Xianxu
Adobe PDF(4757Kb)
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View/Download:51/2
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Submit date:2023/04/20
Shock wave
Hypersonic turbulent
boundary layer
Heat transfer
Skin friction decomposition
Direct numerical simulation
机体尾缘形状对高压捕获翼构型亚声速特性影响
期刊论文
航空学报, 2023, 卷号: 44, 期号: 06, 页码: 10.7527/S1000-6893.2022.27215
Authors:
王浩祥
;
肖尧
;
张凯凯
;
李广利
;
常思源
;
田中伟
;
崔凯
Adobe PDF(2111Kb)
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Submit date:2022/10/17
高压捕获翼
亚声速
流动特性
流动分离
数值模拟
一种并联两级入轨飞行器纵向分离方案的数值研究
期刊论文
航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634
Authors:
王粤
;
汪运鹏
;
王春
;
姜宗林
Adobe PDF(4901Kb)
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View/Download:603/90
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Submit date:2022/07/11
两级入轨
高超声速
纵向分离
气动干扰
非定常流动
基于主动射流控制的高超声速进气道再起动性能研究(英文)
期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:
靳一超
;
姚卫
Adobe PDF(1844Kb)
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Submit date:2023/02/09
高超声速进气道
不起动
再起动
主动射流
流动控制
Experimental study of hysteresis and catastrophe in a cavity-based scramjet combustor
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 10, 页码: 118-133
Authors:
Zhang X(张旭)
;
Zhang QF(张启帆)
;
Wu ZJ(吴振杰)
;
Yue LJ(岳连捷)
;
Gao ZB(高占彪)
;
Luo WH(罗苇航)
;
Chen H(陈昊)
Adobe PDF(4834Kb)
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Submit date:2023/07/17
Catastrophe
Cavity-based scramjet
Flame stabilization
Flame/shock interaction
Hysteresis
基于高温真实气体效应的双锥磁流体流动控制
期刊论文
航空学报, 2022, 卷号: 43, 期号: S2, 页码: 79-91
Authors:
罗凯
;
汪球
;
李进平
;
赵伟
Adobe PDF(1945Kb)
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Submit date:2023/02/09
磁流体
流动控制
双锥流动
高温真实气体效应
洛伦兹力
基于高温真实气体效应双锥MHD流动控制研究
期刊论文
航空学报, 2022, 页码: 14
Authors:
罗凯
;
汪球
;
李进平
;
赵伟
Adobe PDF(1326Kb)
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Submit date:2022/10/17
磁流体
流动控制
双锥流动
高温真实气体效应
洛伦兹力