摘要
为了满足民机溅水后缘襟翼结构安全的设计要求,本文通过参考大量国内外研究者的文献,首先阐述了飞溅类型,建立飞溅角计算模型,通过国外溅水试验,对后缘襟翼的溅水载荷进行计算。得到民机后缘襟翼溅水计算方法,在型号上成功得到了应用,对初期结构设计提供了指导。
In order to meet the requirements of structure safety of trailing edge flap when sprays produced by aircraft tyres running in water or slush,sprays model and load of trailing edge flap are study through theoretical analysis based on research references and tests. The principle and the method of sprays analysis are successfully applied on the aircraft and supply references to structure design in the preliminary design stage.
出处
《科技视界》
2015年第28期5-8,共4页
Science & Technology Vision
关键词
后缘襟翼
溅水
分析
Trailing edge flap
Spray
Analysis
