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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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岳连捷 [14]
张新宇 [13]
张启帆 [4]
肖雅彬 [3]
贾轶楠 [3]
崔季平 [2]
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Indexed By:CSCD
Author:岳连捷
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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
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:271/41
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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
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH(马生虎)
;
Zhang QF(张启帆)
;
Zhang, Peng
;
Zhang XY(张新宇)
Adobe PDF(3937Kb)
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Submit date:2021/03/30
Adverse pressure gradient
Back pressure
Hysteresis effects
Non-uniform flow
Shock train
斜爆轰波的波角和法向速度-曲率关系初步探究
期刊论文
航空学报, 2020, 卷号: 41, 页码: 123701
Authors:
杨理
;
岳连捷
;
张新宇
Adobe PDF(5656Kb)
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Submit date:2021/01/29
内压缩波系对高超声速进气道自起动性能影响研究
期刊论文
实验流体力学, 2019, 卷号: 33, 期号: 03, 页码: 60-67
Authors:
贾轶楠
;
张启帆
;
仝晓通
;
岳连捷
;
张新宇
Adobe PDF(2765Kb)
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Submit date:2019/09/12
自起动性能
肩部膨胀扇
侧压式
边界层厚度
几何喉道
气动喉道
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
Adobe PDF(1675Kb)
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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
隔离段抽吸引起的激波迟滞现象研究
期刊论文
推进技术, 2017, 卷号: 38, 期号: 04, 页码: 732-739
Authors:
马生虎
;
岳连捷
;
贾轶楠
;
肖雅彬
;
张新宇
Adobe PDF(1677Kb)
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Submit date:2017/12/22
超燃冲压发动机
隔离段
激波反射迟滞
边界层分离迟滞
H_2O/CO_2污染对RP-3航空煤油着火特性的影响
期刊论文
推进技术, 2015, 卷号: 36, 期号: 3, 页码: 336-344
Authors:
梁金虎
;
王苏
;
张灿
;
张胜涛
;
岳连捷
;
范秉诚
;
张新宇
;
崔季平
Adobe PDF(1583Kb)
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Submit date:2015/12/25
污染效应
着火延时
煤油
H2o
Co2
激波管
高超声速进气道快速破膜开启的流动特性
期刊论文
航空学报, 2015, 卷号: 36, 期号: 6, 页码: 1795-1804
Authors:
徐骁
;
岳连捷
;
卢洪波
;
肖雅彬
;
张新宇
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Adobe PDF(711Kb)
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View/Download:337/81
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Submit date:2015/12/25
高超声速进气道
破膜开启
非定常效应
激波边界层相互作用
分离流