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Computational Analysis and Prototype Experiment of anomaterial for Aircraft Wing Inboard Flap in Aerospace Industry

机译：航空航天飞机机翼内侧皮瓣材料的计算分析与原型实验

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摘要

The aircrafts fly at both high altitude and fast airspeed in the air but needs slow airspeed in order to land safely. To increase aircraft fly efficiency, the material and design of wing inboard flap should be carefully engineered to provide aircraft with high speed flight in the air but keep strong lift with lower airspeed in order to safely land to the ground. The wing inboard flap is a critical part for the aircrafts and the previous researches showed that the damaged inboard flap can lead aircraft function failure and even cause fatal accidents in the flight and landing processes. Since the defects in wing inboard flap can cause potential safety hazards, the strong inboard flap materials and good inboard flap design to keep safe flight is very important. This paper studies and analyzes the nanocoated material applied in the design and development of aircraft wing inboard flap by using computer-aided 3D modeling, numerical simulation, and prototype experiment to improve current and future wing inboard flap design and development.
机译：飞机既可以在高空飞行，又可以在空中以高空速飞行，但是需要缓慢的空速才能安全着陆。为了提高飞机的飞行效率，机翼内侧襟翼的材料和设计应经过精心设计，以使飞机能够在空中高速飞行，但在较低的空速下保持强劲的升力，以便安全着陆。机翼内侧襟翼是飞机的关键部分，先前的研究表明损坏的内侧襟翼会导致飞机功能失效，甚至在飞行和着陆过程中造成致命事故。由于机翼内侧襟翼的缺陷可能导致潜在的安全隐患，因此坚固的内侧襟翼材料和良好的内侧襟翼设计以保持安全飞行非常重要。本文通过计算机辅助3D建模，数值模拟和原型实验研究和分析了用于飞机机翼内侧襟翼设计和开发的纳米涂层材料，以改善当前和未来机翼内侧襟翼的设计和开发。

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    Li Jeremy (Zheng);

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  • 年度 2016
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