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| Numerical Study of Camber and Stagger Angle Effects on the Aerodynamic Performance of Tandem-Blade Cascades 会议论文
作者: Behshad Ghazanfari, Mahdi Nili-Ahamadabadi, Ashkan Torabi-Farsani, and Mohammad Hossein Noorsalehi
  收藏 | 浏览/下载：17/0 | 提交时间：2017/08/16 |
| Alleviation of Shock-Wave Effects on a Highly Loaded Axial Compressor Through Novel Blade Shaping 会议论文
作者: Alistair John, Shahrokh Shahpar, and Ning Qin
收藏 | 浏览/下载：17/0 | 提交时间：2017/08/16 |
| Effects of Total Pressure Inlet Distortion on Transonic Fan Blade Wake Properties 会议论文
作者: Anthony M. Ferrar, William Schneck III, Alfred Wicks, and Walter O’Brien
收藏 | 浏览/下载：10/0 | 提交时间：2017/08/16 |
| Effects of Rotor Tip Blade Loading Variation on Compressor Stage Performance 会议论文
作者: Aniwat Tiralap, Choon S. Tan, Christian Cornelius, Eric Donahoo, and Matthew Montgomery
收藏 | 浏览/下载：11/0 | 提交时间：2017/08/16 |
| Effect of Ice and Blade Interaction Models on Compressor Stability 会议论文
作者: Swati Saxena, George T. K. Woo, Rajkeshar Singh, Andrew Breeze-Stringfellow, Tsuguji Nakano, and Peter Szucs
收藏 | 浏览/下载：6/0 | 提交时间：2017/08/16 |
| The Effect of an Eroded Leading Edge on the Aerodynamic Performance of a Transonic Fan Blade Cascade 会议论文
2014
作者: J. Klinner; R. Schnell; S. Grund; M. Beversdorff; A. Giebmanns
收藏 | 浏览/下载：7/0 | 提交时间：2015/01/07 |
| Riblet Application in Compressors: Towards Efficient Blade Design? 会议论文
2014
作者: M. Terhorst; S. Grund; W. Hage; A. Hergt; W. Steinert
收藏 | 浏览/下载：7/0 | 提交时间：2015/01/07 |
| Experimental Study of Effects of Bowed Blade on the Flow Field in a Cantilevered Stator Passage 会议论文
2014
作者: Jun Hu; Ju Luo; Baofeng Tu; Zhiqiang Wang
收藏 | 浏览/下载：16/0 | 提交时间：2015/01/07 |
| Effects of Curvature Continuity of Compressor Blade Profiles on Their Performances 会议论文
2014
作者: Chunwei Gu; Yin Song
收藏 | 浏览/下载：11/0 | 提交时间：2015/01/07 |
| Multi-Objective Constrained Aero-Mechanical Optimization of an Axial Compressor Transonic Blade 会议论文
Copenhagen, Denmark, 2012-06-11
作者: Stefano Piola; Federico Bonzani; Andrea Silingardi; Pio Astrua
收藏 | 浏览/下载：9/0 | 提交时间：2012/08/13 |
