固体火箭发动机内孔星形药柱采用J准则时在不同条件下的解析设计

ANALYTICAL DESIGN BASED ON PRINCIPLE J* FOR INTER-NAL BURNING STAR GRAINS OF SOLID ROCKETSUNDER DIFFERENT CONDITIONS

本文是文献[2]、[3]的系统化发展,在限制侵蚀燃烧的产准则下,建立了更完善的设计方程式;给出了在不同的战术技术要求下,设计方程式的组合及计算机解法,全面发展并最后完善了原著[2]、[3]的解析设计法。 /

This paper is the systematic development of [2] and [3] . Based on the printiple J* of the limitation of scouring combustion, we have established more perfect design cquation series. The combination of design equations and the computer programs under different tactical requirements have also been given in this paper. Thus it makes the analytical design shown in my original works of [2] and [3] to have universal applicability and completeness.