通风舱室爆炸准平稳压力的计算方法

Pengduo Zhao, Haojie Wang, Zhipeng Du, Xiaobin Li
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引用次数: 0

摘要

密闭舱内发生爆炸,会使舱内气体压力急剧上升,对舱内结构造成严重破坏。准静压力由于持续时间长、冲量大,对整个客舱结构强度的破坏起主要作用。横向舱壁上的排气孔可以有效地引导能量释放到其他位置,减少对机舱的破坏。本文研究了带通风的舱室爆炸过程中产生的准静压力。根据质能守恒原理,将带排气的舱室爆炸模型转化为等效高压气体释放模型,模拟舱室爆炸的初始瞬时状态,并通过有限元计算验证了两种模型在预测准定压时的等效性。通气孔爆炸时的整个气体流动过程分为两部分:舱内气体流向通气孔和通气孔向大气的气体流动。利用伯努利方程和理想气体等熵压缩公式,改进了舱室通风爆炸准平稳压力的近似解析预测方法,并将改进计算方法的结果与数值模拟方法的结果进行了比较,验证了改进计算方法的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Calculation Method for the Quasi-Stationary Pressure in Cabin Explosion With Venting
The explosion in the closed cabin will cause a sharp rise in cabin gas pressure, which will cause serious damage to the cabin structure. The quasi-stationary pressure, due to its long duration and large impulse, plays a major role in the destruction of the structural strength of the entire cabin. The venting holes on the transverse bulkheads can effectively guide the release of energy to other locations, reducing the damage to the cabin. In this paper, the quasi-stationary pressure generated during cabin explosion with venting is studied. According to the conservation of mass and energy, the cabin explosion model with venting is transformed into an equivalent high pressure gas release model to simulate the initial instantaneous state of cabin explosion, and it is verified by finite element calculation that the two models are equivalent in predicting quasi-stationary pressure. The entire gas flow process during the exploding with venting holes is divided into two parts: the gas flow in the cabin to the venting hole and the venting hole to the atmosphere. An approximate analytical method for predicting quasi-stationary pressure generated during cabin explosion with venting is improved by using Bernoulli equation and isentropic compression formula of ideal gas, and the results of the improved calculation method are compared with the results obtained by the numerical simulation method to verify its validity.
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