03.4 - Applied Aerodynamics
RESEARCH ON THE INFLUENCE OF FLIGHT ATTITUDE ON UNILATERAL MISSILE SEPARATION FROM EMBEDDED BAY
Z. Wei, China
By coupling of solving unsteady N-S equations in flow field and 6-DOF equations of rigid body based on dynamic embedded mesh, the accurate simulation of embedding separation is realized, and the influence of different flight attitudes of the aircraft on the missile separation is researched in which the missile was mounted in right side and the left side was empty.