ABOUT LARGE U SHAPE WING OF GLIDER AIRPLANE MODEL

被引:0
作者
Arghir, George [1 ]
机构
[1] Tech Univ Cluj Napoca, Fac Mat Engn & Environm, Cluj Napoca, Romania
来源
ACTA TECHNICA NAPOCENSIS SERIES-APPLIED MATHEMATICS MECHANICS AND ENGINEERING | 2019年 / 62卷 / 01期
关键词
U large wing; V wing; coefficient of restauration;
D O I
暂无
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The U large wing is a new proposed shape of the glider airplane model wing. Its stability is compared to V wing. U large wing I/II has increased stability as the tilting angle increases, less than for V wing I/ II. Its strong instability is at beta = 90 degrees, when the wing is in vertical position. Its stability range is larger than for V wing. The V wing has the stability range limited by a, being 90 degrees - alpha., where a is the angle between wings and horizontal line, in normal flight. beta is the tilting angle for the wing. It can be trigonometric or anti trigonometric rotation, seen from the tale.
引用
收藏
页码:19 / 22
页数:4
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