운반용 발사체로부터 분리되는 다 물체의 운동 예측

초록

Numerical simulations have been performed to predict the 6 D.O.F. motions of multiple bodies ejecting from a missile in supersonic flight. Roe's flux difference splitting scheme, and Chimera overset technology have been applied to obtain the multi body flow field solutions. Computed results of several separation scenarios have provided significant physical insight into the motion characteristics of multiple bodies and the complex unsteady flow field.