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Updated: Jun 23, 2025

Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods
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Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods

Published on: April 23, 2018

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基于二维翼翼的可变翼尾翼的设计和验证

Jin Zhou1, Xiasheng Sun1,2, Qixing Sun1

  • 1Chinese Aeronautical Establishment, Beijing 100012, China.

Biomimetics (Basel, Switzerland)
|June 26, 2024
PubMed
概括

这项研究提出了一种基于链接的新型设计,用于飞机机翼的可变斜坡尾翼,这对于绿色航空至关重要. 创新的机械设计成功地满足了在相当大的空气动力学负载下强度要求.

关键词:
瓦特的I机制.全尺寸的试验件.在地面验证验证.尾行边缘的尾行边缘是什么可变的坎伯翼变量.

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