شماره ركورد كنفرانس :
2912
عنوان مقاله :
Parametric study on buckling of composite cylinder shells under axial and torsion loading
پديدآورندگان :
Mehrabi M نويسنده Genetics Group, Jehad Daneshgahi University, Yazd, Iran. , Shahramyar M. نويسنده , Soroush A نويسنده
تعداد صفحه :
2
كليدواژه :
Bukling Load , Composite cylinder , Axial and Tensional Loading , fiber orientation
عنوان كنفرانس :
مجموعه مقالات چهارمين كنفرانس بين المللي كامپوزيت
زبان مدرك :
فارسی
چكيده فارسي :
Abstract- In the present research, the effects of fiber orientation in buckling load of composite cylinders shells in different lay-up sequences under axial and torsion loading have been investigated. A parametric study for different lay-up sequences is given with changing with 5 Degree step the fibre orientation from 0 to 90 degree. A numerical simulation using FE commercial program Abaqus was used to acquire critical buckle load according to Eigenvalue buckling prediction method. First the validity of the results is checked by making comparison with experiments references and very good agreement is achieved. Keywords - , , ,
شماره مدرك كنفرانس :
3816829
سال انتشار :
1394
از صفحه :
1
تا صفحه :
2
سال انتشار :
0
لينک به اين مدرک :
بازگشت