报告题目：

New Concept Airplanes, High Order Schemes and Fluid-Structural Interaction, New Algorithm based on Cartesian Grid

报告人: Associate Prof. Zha Gecheng

Director of CFD and Aerodynamics Lab.

Dept. of Mechanical & Aerospace Engineering University of Miami

时间：2010年1月21日(星期四)下午3：00

地点：力学所1号楼小礼堂内会议室

摘要：

The new concept airplane will introduce a supersonic bi-directional flying wing and a co-flow jet transonic airplane. The high order schemes will include a new 7th order WENO scheme and 6th order conservative central differencing. The Fluid-Structural Interaction will be on using DES for transonic limited cycle oscillation and AGARD Wing flutter. Lastly, a new hybrid algorithm of Cartesian grid and body fitted grid is introduced.

欢迎大家踊跃参加!