Unsteady Separation Simulation of Missile by Using Moving Grid

움직이는 격자계를 이용한 유도탄의 비정상 분리 유동해석

  • Published : 2007.06.29

Abstract

Missile staging and airframe separation simulation were performed by using a numerical technique for simulating the dynamics of multiple moving bodies. A 6DOF model is fully integrated into the CFD solution procedure to determine the body dynamics. Chimera grid technique offered efficient CFD simulation of multiple moving bodies. Through this simulation the safety of deployed staging and airframe separation mechanism was verified.

Keywords

References

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