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Design method of supplemented surface on airport's high-speed exit(PDF)

长安大学学报(自然科学版)[ISSN:1006-6977/CN:61-1281/TN]

Issue:
2012年03期
Page:
45-48
Research Field:
道路工程
Publishing date:

Info

Title:
Design method of supplemented surface on airport's high-speed exit
Author(s):
PENG Yin1 CHONG Xiao-lei1 YUAN Jun-shan2 XU Jian-hui2
1. School of Aeronautics and Astronautics Engineering, Air Force Engineering University, Xi'an 710038, Shaanxi, China; 2. Unit 93501 of the PLA, Beijing 100000, China
Keywords:
road engineering airport pavement high-speed exit supplemented surface center of main gear configuration
PACS:
U412.3; TU279.71
DOI:
-
Abstract:
In order to give a design reference for the supplemented surface on military airport high-speed exit, the rules of the center of the main landing gear traces circular and straight were analyzed, the correlation curve of the plane's front wheel steering angle and the offset value of the center of the main landing gear traces was obtained, the rules of the center of main landing gear's operating on bend were determined. According to the needs of the aircraft operation, combined with the requirements of the military aircrafts' sliding with the minimum speed, and based on the operation rules, the design procedures for the supplemented surface of high-speed exit to suit for military aircraft were put forward. A supplemented surface for a specific kind of aircraft was designed by this method. The result shows that the method can accurately reflect the operation traces of military aircraft running on bend. 2 tabs, 6 figs, 6 refs.

References:

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Memo

Memo:
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Last Update: 2012-08-20