飞机地面滑行过程中最短滑跑距离的确定  

The Optimal Taxi-Distance Determining on Aircraft Take-off and Landing

作　　者：邓扬晨[1] 张爽[1] 陈华[2] 马明亮[3] 

机构地区：[1]沈阳飞机设计研究所一部,辽宁沈阳110035 [2]西北工业大学机电工程学院,陕西西安710072 [3]九江学院材料科学与工程学院,江西九江332005

出　　处：《航空计算技术》2006年第1期71-74,78,共5页Aeronautical Computing Technique

基　　金：航空科学基金(03B53003);辽宁省科学技术航空专项基金(20044007)

摘　　要：为了确定飞机地面滑行过程中的最短滑跑距离,本文通过优化的方式给出发动机的最佳安装角和飞机地面滑跑的最佳攻角以及前起落架的最佳凸伸量;并通过算例给出了高度与地面滑跑距离之间的关系曲线,为飞机在高原机场的起降提供一定的参考;最后,综合全文给出四点结论。In order to determine the taxi -distance in the process of aircraft taking off and landing, first through optimization, we gave the engine＇s optimal fixing angle and the optimal attack angle of ground running as well as the optimal stretching of front landing gear in this paper. Then by numerical example of aircraft conceptual design, we offered the relationship between the height of airfield and ground running distance, for which was the reference taking off and landing on plateau airport. Finally four conclusions were drawn by authors.

关 键 词：飞行器 起飞 着陆 滑跑距离 优化 

分 类 号：O242[理学—计算数学]