关键词: 固体火箭发动机, 两相流, 理想型面, 曲线造型, 数值模拟, 塞式喷管

Abstract:

This paper proposes an improved Angelino method and an improved “Parabola plus Cubic” curve method to design the solidpropellant axial plug nozzle on the assumption of constant velocity drag coefficient for two-phase flow. The performances of the two-phase plug nozzles designed by the improved methods are computed.

Key words: solidpropellant , rocket , motor,  , two-phase , flow,  , ideal , contour,  , curve , design,  , numerical , simulation,  , plug , nozzle