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Theoretical Rationality Analysis of the Force Equation Due to Aircraft Strike

机译:飞机撞击造成的力方程的理论理性分析

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The traditional structural analysis of the containment building subjected to aircraft impact forces is often performed using the uncoupled calculation method, which directly applies the reaction force versus time curve to the containment building. The difference between the displacement of containment building calculated with the uncoupled method and that calculated using the coupled method is of significant. In order to explain the cause of this problem, the theoretical analysis of the simplified model are presented. The aircraft is simplified as a single-degree-of-freedom (SDOF) model. Three containment building models with different degree of simplification are analyzed, including the elastic free model, elastic clamped model and elastoplastic model with fixed support. The surfaces of these models are perpendicular to the direction of impact. The results indicate that due to Riera assumes the target to be rigid with fixed support, the impact force equation will lead to the calculation time difference between uncoupled method and coupled method. And the difference of time will cause the different displacement of the containment building by order of magnitude. Riera's impact force equation is widely used in the uncoupled method, so its rationality has great significance. This work points out the shortcoming of this equation, and provides a theoretical support for the improvement of the containment structural performance analysis method due to aircraft strike, also for the subsequent improvement of the impact force equations.
机译:经常经受飞机冲击力的传统结构分析通常使用未耦合计算方法进行,该计算方法直接将反应力与时间曲线施加到容纳建筑物。用解耦方法计算的容纳建筑物的位移与使用耦合方法计算的差异有显着性。为了解释这个问题的原因,提出了简化模型的理论分析。该飞机被简化为单一程度自由度(SDOF)模型。分析了具有不同简化程度的三种容纳建筑模型,包括具有固定支撑的弹性自由模型,弹性夹紧模型和弹塑性模型。这些模型的表面垂直于撞击方向。结果表明,由于RIERA假设具有固定支撑的目标刚性,冲击力方程将导致解耦方法与耦合方法之间的计算时间差。时间的差异将导致遏制建筑的不同位移按级别级。 RIERA的冲击力方程被广泛应用于解耦方法,因此其合理性具有重要意义。这项工作指出了该等式的缺点,并提供了改善由于飞机撞击引起的容纳结构性能分析方法的理论支持,也用于随后改善冲击力方程。

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