首页> 外文会议>ESA Symposium on European Rocket and Balloon Programmes and Related Research >RESEARCH ON THE STRUCTURAL SAFETY OF THE STRATOSPHERIC AIRSHIP BASED ON MULTI-PHYSICS COUPLING CALCULATION
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RESEARCH ON THE STRUCTURAL SAFETY OF THE STRATOSPHERIC AIRSHIP BASED ON MULTI-PHYSICS COUPLING CALCULATION

机译:基于多物理耦合计算的平流层飞艇结构安全研究

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As a large-scale flexible inflatable structure by a huge inner lifting gas volume of several hundred thousand cubic meters, the stratospheric airship's thermal characteristic of inner gas plays an important role in its structural performance. During the floating flight, the day-night variation of the combined thermal condition leads to the fluctuation of the flow field inside the airship, which will remarkably affect the pressure acted on the skin and the structural safety of the stratospheric airship. According to the multi-physics coupling mechanism mentioned above, a numerical procedure of structural safety analysis of stratospheric airships is developed and the thermal model, CFD model, finite element code and criterion of structural strength are integrated. Based on the computation models, the distributions of the deformations and stresses of the skin are calculated with the variation of day-night time. The effects of loads conditions and structural configurations on the structural safety of stratospheric airships in the floating condition are evaluated. The numerical results can be referenced for the structural design of stratospheric airships.
机译:由于大型柔性充气结构,通过巨大的内部升降气体容积数十万立方米,地铁的流程主义飞艇的热特性在其结构性能下起着重要作用。在浮动飞行期间,组合热条件的日夜变化导致飞艇内流场的波动,这将显着影响对皮肤上的压力和平流层飞艇的结构安全性。根据上述多物理耦合机制,开发了平流层飞艇结构安全分析的数值过程,集成了热模型,CFD模型,有限元码和结构强度的标准。基于计算模型,通过日夜时间的变化计算皮肤变形和应力的分布。评估了载荷条件和结构配置对浮动条件中平流层飞艇结构安全的影响。可以参考数字结果,用于平流层飞艇的结构设计。

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