固体火箭发动机喷管型面的研究进展*

doi:10.13385/j.cnki.vacuum.2020.01.08

Abstract

Abstract: The counter design of solid rocket engine nozzle profile is directly related to nozzle efficiency and thrust, which is an important research topic in the design of nozzle. In this paper, the research progress on the nozzle profile of solid rocket motor has been reviewed from the aspects of nozzle design method, profile parameter optimization and nozzle fluid-solid coupling analysis. The nozzle design methods such as the direct optimization method, length-shorted nozzle, the six-time Bézier curve, Bi-cubic spline, the B-Spline curve and the method of characteristics are summarized. The applications of computational fluid dynamics and stochastic optimization methods in solid rocket motor design optimization are introduced. The fluid-solid thermal coupling problem of solid rocket engine nozzle has been analyzed. The classical computational fluid dynamics algorithm, characteristic-based split finite element algorithm and a lattice Boltzmann algorithm are used in the study of fluid-solid coupling problems.

Key words: solid rocket motor, counter design, parametric optimization, fluid-solid coupling problems

CLC Number:

TB75

YANG Fei, LI Zhen-hai, LI Jian-chang. Latest Studies on Solid Rocket Engine Nozzle Profile[J].VACUUM, 2020, 57(1): 40-47.

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Latest Studies on Solid Rocket Engine Nozzle Profile

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