| 摘要: |
| 针对机翼受力对模型飞机的影响，本文对模型飞机机翼的升力和阻力进行受力分析和ANSYS的仿真分析，通过分析可以对机翼进行升力和阻力的准确计算，从而提出最佳设计方案。通过ANSYS的仿真分析可以确定机翼变形时的临界状态，从而确定机翼的临界受力。 |
| 关键词: 模型飞机 机翼 受力分析 仿真 |
| 基金项目: |
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| Force Analysis and Simulation of Model Airplane Wings |
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Tian Xiaofei Yang Pingping Wang Zirong Li Yuan Qin Hao
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Mechanics Academy, North University of China (Shuozhou Campus), Shuozhou 036000
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| Abstract: |
| According to the effects of the wing loading on the model airplane, the force analysis and ANSYS simulation analysis are carried out for the lift and drag force of model airplane wing. The optimal design scheme is put forward through the accurate calculation of the lift and drag force of model airplane wing. The critical state of the wing deformation is determined on the base of ANSYS simulation analysis, thereby the critical stress of the wing can be ascertained. |
| Key words: model aircraft wing force analysis simulation |
