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浏览/检索结果: 共7条，第1-7条 帮助 限定条件 专题：北京大学    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 Influence of coupled boundary layer suction and bowed blade on flow field and performance of a diffusion cascade 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2017 Cao Zhiyuan; Liu Bo; Zhang Ting; Yang Xiqiong; Chen Pingping 收藏  |  浏览/下载：6/0  |  提交时间：2017/12/03 Axial compressor  Boundary layer suction  Bowed blade  Corner separation  Coupled method  Passage vortex   Comparison of aerodynamic characteristics between a novel highly loaded injected blade with curvature induced pressure-recovery concept and one with conventional design 期刊论文 中国航空学报（英文版）, 2017 Zhiyuan CAO; Chao ZHOU; Zhili SUN 收藏  |  浏览/下载：6/0  |  提交时间：2017/12/03 Axial compressor Air injection Curvature induced ‘Shock’ Flow control Separation  Axial compressor  Air injection  Curvature induced ‘Shock’  Flow control  Separation  COMPRESSOR  AIRFOILS  FLOW   Heat Transfer of Winglet Tips in a Transonic Turbine Cascade 期刊论文 JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2017 Zhong, Fangpan; Zhou, Chao; Ma, H.; Zhang, Q. 收藏  |  浏览/下载：5/0  |  提交时间：2017/12/03 AEROTHERMAL PERFORMANCE  TRANSFER COEFFICIENTS  BLADE TIPS  SQUEALER  GEOMETRY  CLEARANCE  LEAKAGE  REGIONS  FLOW   Heat Transfer of Winglet Tips in a Transonic Turbine Cascade 会议论文 Zhong, Fangpan; Zhou, Chao; Ma, H.; Zhang, Q. 收藏  |  浏览/下载：4/0  |  提交时间：2017/12/03 AEROTHERMAL PERFORMANCE  TRANSFER COEFFICIENTS  BLADE TIPS  SQUEALER  GEOMETRY  CLEARANCE  LEAKAGE  REGIONS  FLOW   Effects of Winglet Geometry on the Aerodynamic Performance of Tip Leakage Flow in a Turbine Cascade 期刊论文 journal of turbomachinery transactions of the asme, 2013 Zhou, Chao; Hodson, Howard; Tibbott, Ian; Stokes, Mark 收藏  |  浏览/下载：4/0  |  提交时间：2015/11/13 HEAT-TRANSFER  SQUEALER TIP  BLADE TIP   Thermal Performance of Cooled Tips in a High-Pressure Turbine Cascade 期刊论文 journal of propulsion and power, 2012 Zhou, Chao; Hodson, Howard; Lock, Gary 收藏  |  浏览/下载：2/0  |  提交时间：2015/11/13 HEAT-TRANSFER COEFFICIENTS  FILM-COOLING EFFECTIVENESS  BLADE TIP  ADIABATIC EFFECTIVENESS  SIDE HOLES  PART II  SQUEALER   Effects of Winglet Geometry on the Aerodynamic Performance of Tip Leakage Flow in a Turbine Cascade 会议论文 Zhou, Chao; Hodson, Howard; Tibbott, Ian; Stokes, Mark 收藏  |  浏览/下载：5/0  |  提交时间：2015/11/13 HEAT-TRANSFER  SQUEALER TIP  BLADE TIP