摘要
本文介绍一种设计固体火箭喷管的新方法。这种方法以拉伐尔喷管内非对称流动理论为基础,首先着眼于减少气动偏心,然后考虑效率。它与传统的方法并不矛盾,而仅是其合理的补充。采用这种设计方法将有助于减少无控火箭的散布。
A new method of the solid propellant rocket nozzle design is presented. The method, based on the theory of non-symmetric flow in Lavol nozzle, aims first at the angle of reducing the gas dynamic misalignment, and then at the angle of efficiency. It doesn't contradict the traditional methods of nozzle design, but supplement them. It will help reduce the dispersion of impact of the free flight rocket.
出处
《兵工学报》
EI
CAS
1984年第4期40-49,共10页
Acta Armamentarii
