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浏览/检索结果: 共6条，第1-6条 帮助 限定条件 专题：工程热物理研究所    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 Non-Axisymmetric End Wall Profiling in Transonic Compressors—Part II: Design Study of a Transonic Compressor Rotor Using Non-Axisymmetric End Walls: Optimization Strategies and Performance 会议论文 ASME:Turbomachinery: Axial Flow Fan & Compressor Aerodynamics, 2009 Steffen Reising and Heinz-Peter Schiffer 收藏  |  浏览/下载：7/0  |  提交时间：2011/11/30 Non-Axisymmetric End Wall Profiling in Transonic Compressors—Part I: Improving the Static Pressure Recovery at Off-Design Conditions by Sequential Hub and Shroud End Wall Profiling 会议论文 ASME:Turbomachinery: Axial Flow Fan & Compressor Aerodynamics, 2009 Steffen Reising and Heinz-Peter Schiffer 收藏  |  浏览/下载：8/0  |  提交时间：2011/11/30 The Effect of Non-Axisymmetric End Wall Profiling on Axial Flow Compressor Aerodynamics: Part II — Multi-Stage HPC CFD Study 会议论文 ASME:Turbomachinery: Axial Flow Fan and Compressor Aerodynamics, 2008 N. W. Harvey and T. P. Offord 收藏  |  浏览/下载：7/0  |  提交时间：2011/11/28 Some Effects of Non-Axisymmetric End Wall Profiling on Axial Flow Compressor Aerodynamics: Part I — Linear Cascade Investigation 会议论文 ASME:Turbomachinery: Axial Flow Fan and Compressor Aerodynamics, 2008 N. W. Harvey 收藏  |  浏览/下载：2/0  |  提交时间：2011/11/28 Some Effects of Non-Axisymmetric End Wall Profiling on Axial Flow Compressor Aerodynamics: Part I — Linear Cascade Investigation 会议论文 2008 N. W. Harvey 收藏  |  浏览/下载：3/0  |  提交时间：2011/11/28 Secondary Flow Reduction in A Nozzle Guide Vane Cascade by Non-Axisymmetric End-wall Profiling 会议论文 ASME, Indianapolis,Indiana, 1999-06-07 J.Yan; D.G.Gregory-Smith; P.J.Walker 收藏  |  浏览/下载：11/0  |  提交时间：2012/07/12