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首页> 外文期刊>International journal of impact engineering >Dynamic responses of a steel-reinforced concrete target impacted by aircraft models
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Dynamic responses of a steel-reinforced concrete target impacted by aircraft models

机译:飞机模型对钢筋混凝土靶的动力响应

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To investigate the characteristics of the impact load for a large commercial aircraft impacting upon a nuclear power plant, an integral test measurement system is developed through the experiments of aircraft models in middle sizes impacting upon a movable steel-reinforced concrete target via a rocket sled loading test platform. Three impact tests with different sizes of the aircraft models were carried out. In all the tests, the flying attitude and velocity of the aircraft models were recorded by a high-speed photography system. The acceleration and velocity time histories of the target were obtained by an acceleration measurement system and a DISAR system, respectively. The computed results of the impact loads calculated by using the measured acceleration and velocity data, respectively, are found to be in good agreement, which verified the reliability of the measurement system. Moreover, the acceleration time histories of the aircraft models were obtained by using the onboard overload storage, and, based on the measured data, the crushing load of the aircraft model can be calculated. On the other hand, the impact load time histories are also calculated by using the modified Riera equation, and the computed results are found to be consistent with that calculated by using the measured acceleration or velocity data of the target. In addition, the correction coefficient a in the modified Riera equation is also determined. Finally, an engineering calculation method and a formula to calculate the aircraft's impact load are proposed, with no need for knowing in advance the aircraft's crushing load distribution data. Moreover, the impact load of an aircraft calculated by using the engineering formula can be used in the evaluation on the impact resistance of the structure in a nuclear power plant, and the evaluation results will be impulse conservative.
机译:为了研究大型商用飞机撞击核电站的撞击载荷的特性,通过试验中型飞机模型并通过火箭雪橇载荷撞击可移动的钢筋混凝土靶,开发了整体测试测量系统测试平台。进行了三种不同尺寸飞机模型的冲击试验。在所有测试中,飞机模型的飞行姿态和速度都是通过高速摄影系统记录的。目标的加速度和速度时间历史分别通过加速度测量系统和DISAR系统获得。发现分别使用测得的加速度和速度数据计算出的冲击载荷的计算结果吻合良好,从而验证了测量系统的可靠性。此外,通过使用机载过载存储器获得了飞机模型的加速时间历史,并且基于测量的数据,可以计算出飞机模型的挤压载荷。另一方面,还通过使用修正的Riera方程来计算冲击载荷时间历史,并且发现计算结果与通过使用测得的目标加速度或速度数据所计算的结果一致。另外,还确定了修正的Riera方程式中的校正系数a。最后,提出了一种工程计算方法和计算飞机冲击载荷的公式,无需事先知道飞机的破碎载荷分布数据。而且,通过工程公式计算出的飞机的冲击载荷可以用于核电厂结构抗冲击性能的评估,评估结果是冲动保守的。

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