使用Matlab Simscape GUI程序可视化直升机动力学课程中教授的基本概念

Andrea Contreras Esquen, Jose Bonilla Martinez, P. Pena, Adeel Khalid, A. Tekes
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引用次数: 0

摘要

传统本科工程课程的学生不仅要与高度复杂的概念作斗争,而且要努力将推导出来的数学方程的物理意义联系起来。在这项研究中,我们开发了一个独立的和用户友好的Matlab Simscape图形用户界面(GUI)程序来可视化在本科水平的直升机动力学课程中提出的概念。开发的GUI程序使学生能够改变叶片的参数,包括旋翼半径,叶片弦,翼型类型,材料性能,飞机的重量,并分析参数对直升机旋翼性能的影响。该程序使用运动动力学来模拟叶片在悬停和向前飞行中的运动。Simspace GUI程序由四个模块组成,从一个简单的梁模型开始。在第一个模块中,叶片被认为是一个简单的悬臂梁,其中输入点载荷垂直向下或以一定角度施加在叶片的尖端。在第二个模块中,力被径向分布的负载所取代,该负载模拟了沿叶片跨度的升力分布。在第三个模块中,分布式负载应用于各种类型的翼型,从对称的NACA翼型到超临界翼型。在第四种模型中,截面速度随方位角的变化而变化,并对前向转子进行了仿真。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Visualizing Fundamental Concepts Taught in Helicopter Dynamics Course Using Matlab Simscape GUI Program
Students taking traditional undergraduate level engineering courses not only struggle with highly complex concepts but also struggle in linking the physical meaning of the derived mathematical equations. In this study, we developed a standalone and user-friendly Matlab Simscape Graphical User Interface (GUI) program to visualize the concepts presented in the undergraduate level helicopter dynamics course. The developed GUI program enables students to change the parameters of the blade including the rotor radius, blade chord, type of airfoil, material properties, the weight of the aircraft and analyze the effect of the parameter on the performance of the helicopter rotor. The program uses motion dynamics to simulate the blade movement in hover and forward flight. The Simspace GUI program is composed of four modules starting with a simplistic beam model. In the first module, the blade is considered as a simple cantilever beam where an input point load is applied at the tip of the blade either vertically down or at an angle. In the second module, the force is replaced by a radially distributed load that simulates lift distribution along the span of the blade. In the third module, the distributed load is applied to various types of airfoils ranging from symmetrical NACA airfoil to supercritical airfoils. In the fourth model, the sectional velocities vary as a function of azimuth, and the forward-moving rotor is simulated.
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