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Study on fluid-structure interaction in liquid oxygen feeding pipe systems using finite volume method

机译:有限体积法研究液氧进料管系统中的流固耦合

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摘要

The fluid-structure interaction may occur in space launch vehicles,which would lead to bad performance of vehicles,damage equipments on vehicles,or even affect astronauts' health.In this paper,analysis on dynamic behavior of liquid oxygen (LOX) feeding pipe system in a large scale launch vehicle is performed,with the effect of fluid-structure interaction (FSI) taken into consideration.The pipe system is simplified as a planar FSI model with Poisson coupling and junction coupling.Numerical tests on pipes between the tank and the pump are solved by the finite volume method.Results show that restrictions weaken the interaction between axial and lateral vibrations.The reasonable results regarding frequencies and modes indicate that the FSI affects substantially the dynamic analysis,and thus highlight the usefulness of the proposed model.This study would provide a reference to the pipe test,as well as facilitate further studies on oscillation suppression.
机译:航天飞机可能会发生流固耦合,从而导致飞行器性能下降,飞行器设备损坏,甚至影响宇航员的健康。本文对液氧供给管系统的动态行为进行了分析。考虑到流固耦合的影响,对大型运载火箭进行了研究。管道系统简化为具有泊松耦合和汇合耦合的平面FSI模型。结果表明,限制削弱了轴向和横向振动之间的相互作用。关于频率和模态的合理结果表明,FSI极大地影响了动力分析,从而突出了所提出模型的实用性。该研究将为管道测试提供参考,并有助于进一步研究振荡抑制。

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  • 来源
    《力学学报:英文版》 |2011年第5期|706-712|共7页
  • 作者

    Xin Wei; Bing Sun;

  • 作者单位

    Institute of Telecommunication Satellite,China Academy of Space Technology,100194 Beijing, China;

    School of Astronautics,Beihang University, 100191 Beijing, China;

  • 收录信息 中国科学引文数据库(CSCD);中国科技论文与引文数据库(CSTPCD);
  • 原文格式 PDF
  • 正文语种 chi
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