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Knowledge Management System of Institue of Mechanics, CAS
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岳连捷 [7]
张新宇 [4]
张启帆 [3]
陈科挺 [2]
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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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View/Download:48/6
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Submit date:2024/02/19
Scramjet inlet
Starting ability
Thermochemical
Work performance
高马赫数超燃冲压发动机技术研究进展
期刊论文
力学学报, 2022, 卷号: 54, 期号: 02, 页码: 263-288
Authors:
岳连捷
;
张旭
;
张启帆
;
陈科挺
;
李进平
;
陈昊
;
姚卫
;
仲峰泉
;
李飞
;
王春
;
陈宏
Adobe PDF(2622Kb)
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View/Download:557/103
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Submit date:2022/03/16
高马赫数
超燃冲压发动机
热化学非平衡
超声速燃烧
低雷诺数流动
激波风洞
飞行试验
Parameters for evaluating the efficiency of inlet compression
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:
Chen KT(陈科挺)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(511Kb)
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Submit date:2022/01/12
Airbreathing engine
Compression efficiency
Compression quality
Inlet
Self-consistency
高速进气道低马赫数不起动特性及马赫数影响规律
期刊论文
推进技术, 2020, 卷号: 42, 期号: 10, 页码: 2207-2217
Authors:
贺理浩
;
张启帆
;
岳连捷
;
张新宇
;
王卫星
;
谭慧俊
Adobe PDF(9600Kb)
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View/Download:256/38
  |  
Submit date:2021/11/12
高速进气道
低马赫数不起动
非定常
气动力
自起动
真实气体效应对Ma10级进气道流动的影响
期刊论文
推进技术, 2019, 卷号: 40, 期号: 05, 页码: 1042-1050
Authors:
张启帆
;
岳连捷
;
贾轶楠
;
张新宇
;
李欣
;
高雄
View
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Adobe PDF(1675Kb)
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View/Download:229/47
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Submit date:2019/09/12
真实气体效应
高马赫数进气道
化学非平衡气体模型
热完全气体模型
前缘钝化
再起动性能
基于工程转捩模型的高超声速进气道特性
期刊论文
北京航空航天大学学报, 2018, 卷号: 44, 期号: 7, 页码: 1408-1418
Authors:
杨慧
;
路文睿
;
李虹杨
;
岳连捷
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Adobe PDF(975Kb)
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View/Download:280/59
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Submit date:2018/10/24
高超声速进气道
转捩模型
飞行高度
湍流度
数值模拟
超燃冲压发动机尾喷管流线追踪设计
期刊论文
推进技术, 2011, 卷号: 32, 期号: 1, 页码: 91-96
Authors:
卢鑫
;
岳连捷
;
肖雅彬
;
张新宇
Adobe PDF(436Kb)
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View/Download:788/234
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Submit date:2012/04/01
三维尾喷管设计
流线追踪
超燃冲压发动机