欢迎访问《空军工程大学学报》官方网站!

咨询热线:029-84786242 RSS EMAIL-ALERT
高原机场飞机着陆滑跑距离计算与分析
DOI:
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

V212.13+1

基金项目:


Calculation and Analysis of Plane's Landing Slipping Length with Full Thrust in Plateau Airfield
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    分析了高原机场的飞机着陆滑跑过程,针对现有方法关于刹车折算摩擦系数的取法不适合计算高原机场飞机着陆滑跑距离的问题,提出了基于速度与摩擦系数关系的刹车摩擦系数计算方法,并考虑了刹车性能、位置的影响,建立了高原着陆数学模型。应用Visual C++语言编写了飞机着陆滑跑距离计算程序,经高原机场测试,Ⅰ型飞机的实测滑跑距离与程序计算距离的最大绝对误差不超过48 m,最大相对误差不超过2.7%;Ⅱ型飞机的实测滑跑距离与程序计算距离的最大绝对误差不超过100 m,最大相对误差不超过4.2%,验证了模型的有效性。结果表明计算模型可用于高原机场着陆滑跑距离计算,模型精度较高,计算范围广。

    Abstract:

    This paper analyzes lading procedure of planes in plateau. In view of taking the converted friction coefficient as its model being not suited for calculating a plane slipping length in plateau airfield by the existing standard method, the paper establishes a mathematic model on a plane landing at plateau airfield under the condition of the influence of break performance and the location, and puts forward a calculation method for friction coefficient based on relationship between the velocity and the friction coefficient in breaking, And the paper writes a plane slipping length progress in language Visual C++. Through on-site test in plateau, maximum absolute error of test length and the computed length measured practically by type-I aircraft does not exceed by 48 m, and its maximum relative error does not exceed by 2.7%; the maximum absolute error of test length and the computed length measured practically by type-II aircraft does not exceed by 100 m, and the maximum relative error does not exceed by 4.2%. The result shows that the calculation model can be used for calculating slipping length in plateau airfield, and the model is high in precision and is wide in calculation scope.

    参考文献
    相似文献
    引证文献
引用本文

蔡良才,张因子,王海服,种小雷,邵斌 ,曲崇杰.高原机场飞机着陆滑跑距离计算与分析[J].空军工程大学学报,2014,(3):5-9

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2015-11-17
  • 出版日期: