24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-2.1.2

DEVELOPMENT OF A MULTI-BLOCK/OVERSET GRID SOLVER

H. R. Kheirandish, J. Nakamichi*
Research Center of Computational Mechanics, Inc., Tokyo, Japan; *Japan Aerospace Exploration Agency

Keywords: SST, unsteady flow, multi-block, overset grid

A new code for steady and unsteady flow simulations based on Multi-Block and Overset grid concept was developed. Its applicability and reliability was verified in different test cases through comparative computations with other methods/others result. In this paper, verifications for multi-block/overset solver and the original code are presented.

view full paper