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浏览/检索结果: 共6条，第1-6条 帮助 限定条件 发表日期：2011     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 Laminar Horse Shoe Vortex for a Triangular Cylinder Flat Plate Juncture 会议论文 RECENT PROGRESSES IN FLUID DYNAMICS RESEARCH - PROCEEDINGS OF THE SIXTH INTERNATIONAL CONFERENCE ON FLUID MECHANICS, 2011-01-01 作者:  Younis, Muhammad Yamin;  Zhang, H.;  Hu, B.;  Sohail, Muhammad Amjad;  Muhammad, Zaka 收藏  |  浏览/下载：4/0  |  提交时间：2020/01/06 juncture flows  horse shoe vortex  PIV  Reynolds number  characteristics frequency   Comparison of Detached eddy simulations with turbulence modeling 期刊论文 World Academy of Science, Engineering and Technology, 2011, 卷号: 50, 页码: 987-993 作者:  Sohail, Muhammad Amjad;  Chao, Yan;  Husain, Mukkarum 收藏  |  浏览/下载：1/0  |  提交时间：2020/01/06 Computational challenges in high angle of attack flow 期刊论文 World Academy of Science, Engineering and Technology, 2011, 卷号: 56, 页码: 1148-1155 作者:  Sohail, Muhammad Amjad;  Chao, Yan;  Ullah, Rizwan;  Younis, Muhammad Yamin 收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06 Effects of Mach Numbers on Side Force, Yawing Moment and Surface Pressure 会议论文 RECENT PROGRESSES IN FLUID DYNAMICS RESEARCH - PROCEEDINGS OF THE SIXTH INTERNATIONAL CONFERENCE ON FLUID MECHANICS, 2011-01-01 作者:  Sohail, Muhammad Amjad;  Muhammad, Zaka;  Husain, Mukkarum;  Younis, Muhammad Yamin 收藏  |  浏览/下载：1/0  |  提交时间：2020/01/06 supersonic  hypersonic  yaw moment coefficient  Mach number  angle of attack   Applications of AUSM+ scheme on subsonic, supersonic and hypersonic flows fields 期刊论文 World Academy of Science, Engineering and Technology, 2011, 卷号: 73, 页码: 242-248 作者:  Younis, Muhammad Yamin;  Sohail, Muhammad Amjad;  Rahman, Tawfiqur;  Muhammad, Zaka;  Bakaul, Saifur Rahman 收藏  |  浏览/下载：9/0  |  提交时间：2020/01/06 Applications of Second Order Low Dissipative Scheme on Hypersonic Configurations 会议论文 2011 INTERNATIONAL CONFERENCE ON AEROSPACE ENGINEERING AND INFORMATION TECHNOLOGY (AEIT 2011), 2011-01-01 作者:  Zaka, Muhammad;  Muhammad, Yamin Younis;  Muhammad, Amjad Sohail 收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06 Hypersonic  Flux difference scheme  Angle of attack  Mach number  numerical dissipation  drag coefficient  minmod limiter