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首页> 外文期刊>Journal of Spacecraft and Rockets >Analytical Methods for Predicting Grain Regression in Tactical Solid-Rocket Motors
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Analytical Methods for Predicting Grain Regression in Tactical Solid-Rocket Motors

机译:战术实心火箭发动机中晶粒回归的预测分析方法

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Algebraic expressions such as those included in this Note represent the foundation of fast analysis for cylindrically perforated solid-rocket-motor grains and combinations of grains. It should be noted that all of the grains mentioned in this Note, except the den-drite, could be represented by the same seven parameters, to be adjusted by any optimization scheme, thereby allowing a tremendous variety of cylindrically perforated grains. If care is taken to maintain a constant web thickness in tapered grains, the equations presented in this Note can be used to model tapered grains accurately, provided that linear averages of geometrically similar cross sections are taken between the two ends of the grain. The versatility and speed with which grain geometries can be explored using this more classical approach to grain design allow the parameter space for motor design to be explored efficiently by design-optimization algorithms.
机译:诸如本注释中所包含的代数表达式表示快速分析圆柱形穿孔的固体火箭发动机晶粒和晶粒组合的基础。应当注意的是,本注释中提到的所有晶粒(除了枝晶)都可以由相同的七个参数表示,可以通过任何优化方案进行调整,从而允许使用多种圆柱状穿孔晶粒。如果注意保持锥形晶粒的腹板厚度恒定,则本说明中提供的方程式可用于精确建模锥形晶粒,前提是在晶粒的两端之间采用几何相似截面的线性平均值。使用这种更经典的晶粒设计方法可以探索晶粒几何形状的多功能性和速度,可以通过设计优化算法有效地探索用于电机设计的参数空间。

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