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Fluid–Structure–Jet Interaction Effects on High-Speed Vehicle Performance and Stability

机译:流体-结构-喷射相互作用对高速车辆性能和稳定性的影响

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摘要

This paper considers the performance and stability of high-speed vehicles due to 7 changes in the vehicle configuration that introduce the interaction of multiple physics. A conventional vehicle model is developed as a reference configuration with a slender fuselage and aft control surfaces. From this baseline, different design characteristics are implemented to create successive vehicle models. The design trends under consideration are structural flexibility, attitude control jets, and removed control surfaces. The combination of these leads to a slender, flexible, cone-cylinder-flare structure with attitude control jets. The added flexibility introduces a coupled fluid-structure interaction, and the attitude control jets interact with external supersonic flow, which leads to a coupled fluid-structure-jet interaction. The complex multiphysics interaction is a nonlinear unsteady phenomenon that must be considered to simulate the vehicle response to various flight conditions and control inputs. This paper presents flight simulation results of multiple vehicle models with varying design characteristics to investigate the effect of multiphysics interactions on the system performance and stability.
机译:本文考虑了由于车辆配置中的7种变化(引入了多种物理相互作用)而导致的高速车辆的性能和稳定性。开发了传统的车辆模型作为具有细长机身和后控制面的参考配置。从该基准开始,将实现不同的设计特征以创建连续的车辆模型。正在考虑的设计趋势是结构灵活性,姿态控制射流和拆除的控制面。这些的结合导致具有姿态控制喷嘴的细长的,柔性的圆锥形喇叭口结构。增加的灵活性引入了耦合的流体-结构相互作用,并且姿态控制射流与外部超音速流相互作用,这导致了耦合的流体-结构-射流相互作用。复杂的多物理场相互作用是非线性的非稳态现象,必须考虑该现象来模拟飞行器对各种飞行条件和控制输入的响应。本文介绍了具有不同设计特征的多种飞行器模型的飞行仿真结果,以研究多物理场相互作用对系统性能和稳定性的影响。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2019年第2期|586-595|共10页
  • 作者单位

    Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA;

    Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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