-
1
Crash Simulation Of A Composite Unmanned Aerial Vehicle Fuselage
Published 2007“…The simulation of the composite fuselage sections was carried out, refined several times and validated with the experimental results. …”
Get full text
Thesis -
2
Crush simulation of woven c-glass/epoxy unmanned ariel vehicle fuselage section
Published 2010“…A quasi-static crush analysis of an unmanned aerial vehicle (UAV) fuselage section made of woven c-glass/epoxy has been conducted using the finite element simulation via ABAQUS. …”
Get full text
Article -
3
Prediction of fatigue life of aluminum 2024-T3 at low temperature by finite element analysis
Published 2020“…The change in material properties at low temperature has always been one of the concerned design factors in aircraft industries. The wings and fuselage are repeatedly exposed to sub zero temperature during cruising at high altitude. …”
Get full text
Article -
4
Experimental and numerical analysis of fatigue life of aluminum Al 2024-T351 at elevated temperature
Published 2020“…Structural parts such as fuselage, wings, aircraft turbines and heat exchangers are required to work safely at this working condition even with decreasing fatigue strength and other properties. …”
Get full text
Article