scholarly journals STRUCTURE POWER AIRCRAFT FUSELAGE 5774 TRAINER

Vortex ◽  
2021 ◽  
Vol 2 (2) ◽  
pp. 82
Author(s):  
Fandi Syafri Pratama

The analysis process using software aims to determine whether an object or material is suitable for use or not before carrying out the manufacturing process. To find out whether the material is strong or not when applied to the aircraft, an analysis is carried out using the ABAQUS CAE 6.14 software. This software will show the stress value that occurs in the sandwich composite structure when it receives the load experienced by the aircraft.

2018 ◽  
Vol 926 ◽  
pp. 57-63
Author(s):  
Hyun Bum Park

This study aims to investigate numerically the damage area of a sandwich composite structure. In this work, the optimal sandwich core modeling method was proposed. This study applied two modeling methods to compare their analysis results for the structural analysis of the sandwich composite structure. Firstly, the modeling of sandwich core structure was performed with laminate modeling method. Secondly, the modeling of core structure was performed with core solid modeling method. The laminate modeling method was compared with the core solid modeling method. For the modeling, a carbon/epoxy composite structure was applied to the face sheet. And a nomex honeycomb core was applied to the core. Finally, comparing the result of modeling as actual shape with the one of virtually applying the thickness and modeling, it was examined that the former had three times more stress than the latter.


1992 ◽  
Vol 30 (5) ◽  
pp. 5-20 ◽  
Author(s):  
Tamon Ueda ◽  
Toshiyuki Shioya

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