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浏览/检索结果: 共5条，第1-5条 帮助 限定条件 专题：北京航空航天大学    第一署名单位    第一作者单位    通讯作者单位     已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Optimization strategy for a single-stage axisymmetric hub endwall in axial compressor by a modified transonic area rule 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 82-83, 页码: 199-209 作者:  Li, Zhiping;  Zhang, Yafei;  Pan, Tianyu;  Lu, Hanan;  Wu, Miao 收藏  |  浏览/下载：11/0  |  提交时间：2019/12/30 Transonic area rule  Optimization design  Compressor hub profile  Blade blockage   Criteria for designing low-loss and wide operation range variable inlet guide vanes 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 80, 页码: 177-191 作者:  Shi, Hengtao;  Liu, Baojie;  Yu, Xianjun 收藏  |  浏览/下载：4/0  |  提交时间：2019/12/30 Variable inlet guide vane  Blade profile loss  Blade surface flow separation  Surface velocity distribution  Axial-flow compressor   Aerodynamic and aeroacoustic redesign of low speed blade profile 会议论文 24th International Congress on Sound and Vibration, ICSV 2017, London, United kingdom, 2017-07-23 作者:  Yan, Y.;  Avital, E.;  Shen, X.;  Zhao, Q.;  Gao, J. 收藏  |  浏览/下载：7/0  |  提交时间：2019/12/30 Constraints and CFD simulation-based parametric reconstruction for 2D blade profile in reverse engineering 期刊论文 PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 页码: 2137-2146 作者:  Zhang, Yun;  Chen, Zhi-Tong 收藏  |  浏览/下载：2/0  |  提交时间：2019/12/30 Turbine blade  reverse engineering  2D-based modeling  parameter constraints  computational fluid dynamics simulation   Leading-edge redesign of a turbomachinery blade and its effect on aerodynamic performance 期刊论文 APPLIED ENERGY, 2012, 卷号: 93, 页码: 655-667 作者:  Zhang, Weihao;  Zou, Zhengping;  Ye, Jian 收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06 Blade profile  Leading edge  Design method  Pressure spike  Separation bubble  Turbomachine