Structural Analysis of Unmanned Aircraft

被引：0
|
作者：
Garcia Sanchez, Geovani Esau [1 ]
Lira Martinez, Manuel Alejandro [1 ]
Uribe Ramirez, Alfonso [1 ]
Villagrana Noris, Carlos [1 ]
Lira Mota, Luis Alonso [1 ]
Ponce Vega, Axel [1 ]
机构：
[1] UACJ, Inst Engn & Technol, Ave Charro 450 Nte Partido Romero, Juarez City 32310, Chihuahua, Mexico
来源：
ADVANCES IN DIGITAL TECHNOLOGIES | 2017年 / 295卷
关键词：
Shear force; bending moment; moment of inertia; structure loads;
D O I：
10.3233/978-1-61499-773-3-151
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
The subject of the paper is to show an optimal aircraft's structure analysis made by students of UACJ using diverse software's such as MATLAB, SolidWorks, Ansys to model and calculate shear force, bending moment, moment of inertia, and all structure loads. The analysis includes wing's structure, fuselage's structure divided by three section, nose, central fuselage and tail, as well as tail assembly. Data in this research show methodologies and tools applied to accomplish the final design.
引用
收藏
页码：151 / 161
页数：11
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