舰载飞机斜板滑跳起飞动力学问题初步研究

THE INITIAL RESEARCH OF CARRIER-AIRCRAFT TAKING-OFF DYNAMIC PROBLEMS

本文根据动力学原理,建立了适于任意斜板形状的滑跳动力学模型,提出了一种起落架载荷的计算方法,进行了斜板滑跳的起飞包线的仿真和分析研究,为进一步研究斜板起飞技术的增益潜力提供了较严格的动力学基础。

This paper deals with the initial research of dynamic problems, and has a research on the aircraft taking-off envelope. It gives a method for calculating the landing gear's loads, and gives some ideas about the optimalizing the design of the ski-jumping runaway board. All this will help the aircraft flight performances research and further researches which take account of the effects of factors such as the carrier's longititude rick and the deck-wind. It also provides a base for optimalizing the design of the ski-jumping board to match the requirement of the carrier and the aircraft.