机构

• 力学研究所 [7]

采集方式

• OAI收割 [7]

内容类型

• 期刊论文 [7]

发表日期

• 2025 [1]
• 2024 [1]
• 2022 [1]
• 2021 [1]
• 2020 [2]
• 2015 [1]
• 更多

学科主题

• Engineerin... [1]
• Engineerin... [1]

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浏览/检索结果: 共7条，第1-7条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Assessment of thermochemical models on nonequilibrium flowfield and radiation in shock-heated nitrogen 期刊论文  OAI收割 COMPUTERS & FLUIDS, 2025, 卷号: 289, 页码: 17 作者:  Zhang YZ(张宇哲);  Hong QZ(洪启臻);  Wang XY(王小永);  Yang, Chao;  Sun QH(孙泉华)   |  收藏  |  浏览/下载：7/0  |  提交时间：2025/02/24 High enthalpy flow  Thermochemical nonequilibrium model  Vibration-dissociation coupling  Nonequilibrium radiative metric   Experimental study on shock interaction control of double wedge in high-enthalpy hypersonic flow subject to plasma synthetic jet 期刊论文  OAI收割 CHINESE JOURNAL OF AERONAUTICS, 2024, 卷号: 37, 期号: 4, 页码: 151-165 作者:  Xie, Xuzhen;  Liu, Qiang;  Zhou, Yan;  Luo, Zhenbing;  Xie,Wei   |  收藏  |  浏览/下载：10/0  |  提交时间：2024/06/11 Hypersonic flow  High-enthalpy flow  Plasma synthetic jet  Shock wave  Flow control   Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文  OAI收割 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339 作者:  Wang, Yunpeng;  Jiang, Zonglin;  Jiang ZL(姜宗林);  Wang YP(汪运鹏)   |  收藏  |  浏览/下载：39/0  |  提交时间：2022/06/10 Boundary layer correction  High-enthalpy flow  Hypersonic wind tunnel  Nozzle design  Real-gas effects   Experimental study on shock wave control in high-enthalpy hypersonic flow by using SparkJet actuator 期刊论文  OAI收割 ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 416-425 作者:  Xie, Wei;  Luo, Zhenbing;  Zhou, Yan;  Gao, Tianxiang;  Wu, Yun   |  收藏  |  浏览/下载：23/0  |  提交时间：2022/10/25 SparkJet  High-enthalpy hypersonic flow  Shock control  Shock-on-shock interaction  Air supply   Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文  OAI收割 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038 作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)   |  收藏  |  浏览/下载：34/0  |  提交时间：2021/03/30 High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique   Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文  OAI收割 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475 作者:  Wang Q(汪球);  Luo K(罗凯);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)   |  收藏  |  浏览/下载：34/0  |  提交时间：2020/08/26 Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow   Development of the detonation-driven expansion tube for orbital speed experiments 期刊论文  OAI收割 Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700 作者:  Jiang ZL(姜宗林);  Wu B(吴波);  Gao YL;  Zhao W(赵伟);  Hu ZM(胡宗民) 收藏  |  浏览/下载：33/0  |  提交时间：2015/04/28 detonation driver  shock-expansion tube  high-enthalpy flow  test flow