Parachute flying physical model and inflation simulation analysis

被引：3
|
作者：
Cao, YH [1 ]
Xu, H [1 ]
机构：
[1] Beijing Univ Aeronaut & Astronaut, Dept Flight Vehicle Design & Appl Mech, Beijing 100083, Peoples R China
来源：
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY | 2004年 / 76卷 / 02期
关键词：
simulation; dynamics; motion;
D O I：
10.1108/00022660410526079
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
By means of establishing parachute's flying physical model, four methods (i.e. tiny segment analysis method, inflating distance method, moment method and simulating canopy shape method) are adopted to analyze and calculate the variations of canopy shape and the parameters of parachute inflation. The results are simply analyzed, and the figures of all the results are compared.
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页码：215 / 220
页数：6
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