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Executive Aircraft Emergency Landing Simulation and Analysis

机译:执行飞机紧急着陆仿真与分析

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摘要

Based on the new 2006 EASA requirements, landing simulationsrnhave been carried out by MSC.Adams resulting in animation moviesrnshowing the landing procedure and loadings on the aircraft structure.rnThose loads were input into MSC.Nastran FEM analyses from whichrnstructure internal loads and displacements were obtained and used asrna basis to substantiate the aircraft structure. It should be noted thatrnimpact loads for short times can also be obtained by FEM programsrnsuch as MSC.Nastran. However this is practically impossible for thernlanding duration time. On the other hand MSC.Adams modeling isrnbased on solid bodies connected by hinges and springs. An effort hadrnto be made in order to fit this simplified model in order to obtain therncorrect results that correlated those of MSC.Nastran at the firstrnimpact. The landing simulation and analysis have been carried out forrnthe following cases: All wheel up, SKEG landing with opened NLGrnand Single MLG landing.
机译:根据2006年EASA的新要求,MSC进行了着陆模拟-亚当斯制作了动画电影,显示了飞机着陆的过程和飞机结构上的载荷-这些载荷被输入到MSC中,Nastran有限元分析从中获得了结构内部载荷和位移,并以asrna为基础来证实飞机的结构。应该注意的是,短时冲击载荷也可以通过FEM程序(例如MSC.Nastran)获得。然而,对于着陆持续时间这实际上是不可能的。另一方面,MSC.Adams建模基于通过铰链和弹簧连接的实体。为了适应该简化模型,需要付出努力,以便获得与第一次冲击时与MSC.Nastran的结果相关的正确结果。在以下情况下进行了着陆仿真和分析:全轮起落,SKEG着陆并打开了NLGrn以及单个MLG着陆。

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