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The equations of the perturbed motion of a rocket as a thin-walled structure with a liquid

机译:带有液体的薄壁结构火箭的摄动运动方程

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摘要

The perturbed motion of a rocket as an elastic thin-walled structure with compartments partially filled with liquid propellant is considered. It is assumed that the normal modes of the hydroelastic oscillations of the rocket are determined under the condition that the velocity potential on the free surface of the liquid is equal to zero and with standard remaining conditions. Certain features of these modes with zero fundamental frequencies are pointed out and the "loss" of mass effect associated with this is explained. Equations are derived for the perturbed motion of a rocket taking account of the hydroelastic oscillations of its structure and the oscillations of the liquid with deviations of the free surface from the equilibrium position under the action of mass forces. The coefficients of these equations, characterizing the relation between the different type of oscillations, are expressed in terms of known hydrodynamic parameters and the values of the oscillation modes at certain points.
机译:考虑了作为弹性薄壁结构的火箭的摄动运动,其隔室部分充满了液体推进剂。假设在液体自由表面上的速度势等于零且标准剩余条件下确定了火箭的水弹性振荡的正常模式。指出了具有零基本频率的这些模式的某些特征,并解释了与此相关的质量效应的“损失”。在质量力的作用下,考虑到火箭的结构的水弹性振荡和液体的振荡,以及自由表面偏离平衡位置的液体的振荡,得出了火箭的扰动方程。这些方程的系数表征了不同类型的振荡之间的关系,用已知的流体动力学参数和某些点处的振荡模式值表示。

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