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A discrete approach to modelling helicopter blade sailing.

机译:建模直升机叶片航行的离散方法。

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摘要

Blade sailing is an aeroelastic phenomenon which can occur during the engage and disengage phases of shipboard operations. This phenomenon is characterized by large blade deflections which are known to occur mainly at low rotor rotational speeds in high wind and sea conditions. Proper examination of this phenomenon requires adequate modelling of many contributing factors, including system dynamics, ship motion, airwake modelling, and aerodynamics. The research encompassed in this thesis sought to achieve a greater understanding of the factors that affect the blade sailing phenomenon through numerical modelling of the system as a whole.;Novel models for system dynamics and ship airwake were developed under this research programme. The dynamic model is comprised of a series of rigid segments, which allows the analyst to completely define the parameters of the system, including number of blades and blade segments. The model also allows the inclusion of coupled stiffness terms, and a method for calculating the equivalent lumped stiffnesses from continuous coupled stiffness distributions. The numerical model was shown to capture non-linear, coupled, flexible beam bending behaviour through validation against published experimental data and analytical models.;The airwake model is based on experimental data, and incorporates changing mean and turbulent flow characteristics over the flight deck in space, time, and with ship deck roll angle. The experimental research showed that ship motion changes the airwake significantly. A novel approach to the modelling of spatially- and temporally-correlated turbulence was developed, which recreates the time history of turbulent velocity fluctuations as experienced by a specific point on the rotating blade.;Using these and previously developed models for ship motion and for blade aerodynamics, a comprehensive model of the system was developed and validated in combined blade sailing-like conditions through experiment. The results of the experiment support the claims that the developed numerical tools capture the important aspects of the blade sailing environment, and that the interplay between the contributors to blade sailing motion is very complex.;The goals of this research, to study the contributors to the blade sailing phenomenon, and to develop validated modelling tools for this purpose, were achieved through this research.
机译:叶片航行是一种空气弹性现象,可能会在舰船操作的接合和脱离阶段发生。这种现象的特征在于叶片偏转大,已知该偏转主要在高风和海况下以低转子转速发生。对这种现象的正确检查需要对许多影响因素进行适当的建模,包括系统动力学,船舶运动,空中唤醒模型和空气动力学。本论文所涉及的研究旨在通过对整个系统的数值模拟来更深入地了解影响叶片航行现象的因素。;在该研究计划下,开发了用于系统动力学和船舶航行的新颖模型。动态模型由一系列刚性段组成,这使分析人员可以完全定义系统参数,包括叶片数量和叶片段。该模型还允许包含耦合刚度项,以及一种用于从连续耦合刚度分布中计算等效集总刚度的方法。数值模型显示出通过针对已发布的实验数据和分析模型进行验证来捕获非线性,耦合的柔性梁弯曲行为;空中唤醒模型基于实验数据,并结合了驾驶舱内变化的平均和湍流特性空间,时间以及与船甲板侧倾角的关系。实验研究表明,船舶运动显着改变了尾流。开发了一种新颖的方法来对空间和时间相关的湍流进行建模,该方法可以重新创建旋转叶片上特定点所经历的湍流速度波动的时间历史;使用这些模型以及先前开发的船舶运动和叶片模型空气动力学方面,开发了系统的综合模型,并通过实验在类似叶片航行的条件下进行了验证。实验结果支持以下观点:已开发的数值工具捕捉了叶片航行环境的重要方面,并且对叶片航行运动的贡献者之间的相互作用非常复杂。通过这项研究实现了叶片航行现象,并为此目的开发了经过验证的建模工具。

著录项

  • 作者

    Wall, Alanna.;

  • 作者单位

    Carleton University (Canada).;

  • 授予单位 Carleton University (Canada).;
  • 学科 Engineering Aerospace.;Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2009
  • 页码 377 p.
  • 总页数 377
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;机械、仪表工业;
  • 关键词

  • 入库时间 2022-08-17 11:37:53

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