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关于刚性-柔性可变曲面翼的空气动力学特性和控制方法的研究
1School of Aeronautic, Northwestern Polytechnical University, Xi'an, 710072, China.
Scientific reports
|July 16, 2025
概括
一种新的刚性-灵活的混合翼设计提高了空气动力性能,显著提高了起重力和减少了阻力. 这种可适应的机翼技术在各种飞行条件下提高了效率,并得到了强大的控制系统的验证.
科学领域:
- 航空航天工程 航空航天工程
- 流体动力学 流体动力学
- 材料科学 材料科学 材料科学
背景情况:
- 传统的飞机机翼在适应不同飞行条件方面存在局限性.
- 材料变形的限制需要创新的翼设计,以提高性能.
- 优化起重与阻力比对于提高空气动力学效率至关重要.
研究的目的:
- 提出和评估一种新的尾翼曲率可变翼段,将刚性和灵活的结构结合起来.
- 为了优化机翼部分的平均线,以获得卓越的刚性-柔性混合变形配置.
- 为了比较混合翼的空气动力学性能与传统的刚性翼.
主要方法:
- 翼段的平均线的参数化为最佳的配置设计.
- 流场计算,以比较混合翼和传统翼的空气动力学特性.
- 开发和测试使用气动肌肉用于灵活翼变形的控制系统.
主要成果:
- 混合动力机翼显著提高了空气动力学性能,升空系数增加了1.66倍,升空阻力比增加了2.86倍.
- 混合机翼需要较小的偏转角度,并且在各种飞行条件下比传统机翼更好地表现出更好的配置.
- 控制系统有效地实现了目标翼曲率,验证了设计的实际适用性.
结论:
- 拟议的刚性-灵活的混合翼提供了卓越的空气动力学效率和适应性.
- 开发的控制系统确保灵活的翼部件的精确变形.
- 这种创新的机翼设计对未来的航空航天应用具有重大潜力.
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