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Updated: Jun 9, 2025

Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods
09:17

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

Published on: April 23, 2018

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对NACA 13112形态变形翼翼的数值调查

Mădălin-Dorin Feraru1, Daniel Măriuța2, Marius Stoia-Djeska1

  • 1Faculty of Aerospace Engineering, National University of Science and Technology Politehnica Bucharest, 060042 Bucharest, Romania.

Biomimetics (Basel, Switzerland)
|October 25, 2024
PubMed
概括

这项研究表明,调整气翼曲率可以改善升力. 在落后边缘附近增加的变形凸增强了空气动力学性能,这对于直升机旋翼叶片和机翼至关重要.

关键词:
在IAR 330 Puma中使用.改变形态的执行力作用力.尾行边缘的门

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