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Mathematical model of one-component gas generator with the control element

机译:具有控制元件的单组分气体发生器的数学模型

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For the analysis of liquid rocket propulsion system with independent fuel supply to the turbine one must simulate the physical processes occurring in each of its elements to determine their dynamic performance. The paper presents the dynamics equations, which describe the processes occurring in the decomposition cell, the nozzle head and the throttle tap. A general differential equation of a one-component gas generator with the throttle is carried out. The mathematical model allows to analyze and identify the main regularities of influence of input variables on the controlled quantity.
机译:为了分析向涡轮机提供独立燃料的液体火箭推进系统,必须模拟其各个部分中发生的物理过程,以确定其动态性能。本文提出了动力学方程,描述了在分解室,喷嘴头和节流阀中发生的过程。进行了带节气门的单组分气体发生器的一般微分方程。数学模型允许分析和识别输入变量对受控量的影响的主要规律。

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