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| 高马赫数超燃冲压发动机燃烧室再生冷却特性研究 学位论文
博士论文，北京: 中国科学院大学, 2023
Authors: 徐雪睿
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高马赫数 超燃冲压发动机 理论分析 解离效率 再生冷却 组合式冷却方法 超临界CO2布雷顿循环 |
| Flexible Electronics: Theory and Method of Structural Design 专著
Wuhan; Beijing; Xi'an:Springer Nature, 2022
Authors: Huang, YongAn; Su YW(苏业旺); Jiang, Shan
Adobe PDF(20110Kb) | Favorite | View/Download：112/1 | Submit date：2023/03/23 |
| Evaluation for Allowable Span Length of a Submarine Pipeline Considering VIV Hysteresis Effect 期刊论文
INTERNATIONAL JOURNAL OF OFFSHORE AND POLAR ENGINEERING, 2021, 卷号: 31, 期号: 3, 页码: 325-332
Authors: Liu J(刘俊); Gao FP(高福平)
 Adobe PDF(286Kb) | Favorite | View/Download：171/33 | Submit date：2021/11/01
Submarine pipelines vortex-induced vibration critical reduced velocity hysteresis effect allowable span length |
| A segmented load spectrum model for high-speed trains and its inflection stress as an indicator for line quality 期刊论文
INTERNATIONAL JOURNAL OF FATIGUE, 2021, 卷号: 148, 页码: 12
Authors: Yuan, Zheng; Chen XJ(陈贤佳); Ma, Lijun; Li, Qiang; Sun, Shouguang; Wei YJ(魏宇杰)
Adobe PDF(4436Kb) | Favorite | View/Download：369/99 | Submit date：2021/06/15
Load spectrum Segmented Weibull distribution Bogie frame High-speed train Inflection stress |
| 近壁面圆柱体涡激振动的临界触发速度及迟滞效应 学位论文
博士论文，北京: 中国科学院大学, 2021
Authors: 刘俊
Adobe PDF(15869Kb) | Favorite | View/Download：291/4 | Submit date：2021/06/03
涡激振动 剪切流 近壁面效应 圆柱体 临界约减速度 迟滞效应 允许悬跨长度 |
| VIV hysteresis effect on the allowable span length of submarine pipelines 会议论文
The 30th International Ocean and Polar Engineering Conference, Shanghai, China, 2020-10-11
Authors: Liu J(刘俊); Gao FP(高福平)
Favorite | View/Download：107/0 | Submit date：2021/01/28 |
| Development progress of coating first wall components with functionally graded W/EUROFER layers on laboratory scale 期刊论文
Nuclear Fusion, 2020, 卷号: 60, 页码: 126004
Authors: Emmerich T; Qu DD(屈丹丹); Ghidersa BE; Lux M; Rey J; Vaßen R; Aktaa J
Adobe PDF(11525Kb) | Favorite | View/Download：208/64 | Submit date：2020/12/18 |
| Investigation on rod-airfoil noise with high-order cell-centered finite difference method and acoustic analogy 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 102, 页码: 22
Authors: Jin Y; Liao F(廖飞); Cai JS; Morris PJ
Adobe PDF(7457Kb) | Favorite | View/Download：254/90 | Submit date：2020/07/06
Aeroacoustics Rod-airfoil configuration Cell-centered finite difference method Delayed detached eddy simulation FW-H acoustic analogy |
| An sequential optimization and aeroelastic constraint transformation method for strength-aeroelastic comprehensive design 期刊论文
JOURNAL OF FLUIDS AND STRUCTURES, 2020, 卷号: 93, 页码: 14
Authors: Zhang ZS; Wang XJ; Chen XJ(陈贤佳)
 View | Adobe PDF(2381Kb) | Favorite | View/Download：296/96 | Submit date：2020/04/07
Comprehensive design Sequential optimization strategy Airplane wing Structural strength Aeroelasticity |
| Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
Authors: Yue LJ(岳连捷); Jia YN(贾轶南); Xu X; Zhang XY(张新宇); Zhang P(张鹏)
View | Adobe PDF(2110Kb) | Favorite | View/Download：378/136 | Submit date：2018/10/30
Inlet restart Cowl shock Shock wave boundary layer interactions |
