초록
In this paper, a DDES analysis on the aerodynamic forces and moments of a generic missile inside a rectangular cavity is presented. First, the implementation of the DDES method into a CFD code is validated by comparing the computational results with the experimental results for unsteady turbulent flows around a cylinder and a back facing step. Second, the unsteady pressure fluctuations inside WICS cavity are computed and compared to the experimental results, which shows a good agreement. The unsteady flow field inside the cavity with the missile is analyzed, and the computational results of the unsteady pressure fluctuation and the force and moment are presented.
출판유형
발행기관
한국전산유체공학회지
박재형
박사과정
이승수
교수
