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BIRD STRIKE STUDIES ON A TRANSPORT AIRCRAFT HORIZONTAL TAIL

机译:在运输机水平尾巴上的鸟罢工研究

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This paper presents bird strike studies on a typical horizontal tail (HT) of a transport aircraft. FAR regulations dictate that the horizontal tail of a transport aircraft be able to sustain impact damage caused by an eight pound bird. Bird strikes on tail planes though less frequent than on windshields and radomes can cause loss of control and eventually lead to accidents. It appears that there are a number of approaches associated with strike modelling including Eulerian and Lagrangian models. Realistic representation of the component is also driven by modelling the nonlinear material behaviour, contact between sub components, self-contact and progressive damage after impact. Thus, impact on lifting and control surfaces of an aircraft while causing local damage make the aircraft vulnerable to progressive system failures. This paper addresses these issues using explicit FEA codes by modelling the bird and the structural component using both Lagrangian and Eulerian models and discusses vulnerability scenarios associated with this kind of impact damage.
机译:本文展示了在运输机的典型水平尾部(HT)上的鸟类罢工研究。潮流规则决定了运输机的水平尾部能够维持由八磅鸟造成的影响损坏。鸟撞在尾翼上虽然比挡风玻璃和放射线在挡风玻璃上的频率较少,可能导致控制丧失并最终导致事故。似乎有许多与罢工建模相关的方法,包括欧拉和拉格朗日模型。通过建模非线性材料行为,副部件与撞击后的自接触和渐进损伤之间的接触来驱动组件的现实表示。因此,对飞机的升降和控制表面的影响,同时导致局部损坏使飞机容易受到渐进式系统故障的影响。本文通过使用拉格朗日和欧拉模型建模鸟类和结构部件来解决这些问题,通过利用拉格朗日和欧拉模型来讨论与这种影响损坏相关的漏洞情景。

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