DocumentCode :
495688
Title :
Composite Strength Scaling Effect Using Progressive Degradation Model
Author :
Rehan, A. ; Grote, K.H.
Author_Institution :
Dept. of Mech. Eng. Design, Otto-von-Guericke Univ. Magdeburg, Magdeburg, Germany
Volume :
2
fYear :
2009
fDate :
March 31 2009-April 2 2009
Firstpage :
1
Lastpage :
5
Abstract :
The strength scaling of composite laminate design has variable response in sub-laminate and ply level scaling methods. The fact is proved experimentally but the reason for this variable response is authentically not known yet. According to dimensional analysis the strength should be invariant to scale and according to Weibull theory strength changes but it does not differentiate between sub-laminate and ply-level scaling method in fact both have different response to strength in reality. The progressive degradation algorithm is used at micro level (constituent material) to investigate the reason for above said variable response in two different scaling methods. The technique showed some good results and it is found that the edge effects causes destruction at edges due to shear stress, in ply level scaled case, causes the strength reduction in simulated samples.
Keywords :
internal stresses; laminates; mechanical strength; Weibull theory; composite laminate design; composite strength scaling effect; dimensional analysis; edge effects; microlevel progressive degradation model; ply-level scaling method; shear stress; sublaminate method; Aerospace industry; Boundary conditions; Composite materials; Computational modeling; Degradation; Laminates; Material properties; Mechanical engineering; Stacking; Testing; Composite; Ply level; Progrssive degradation model; Scaling; Strength; Sublaminate;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Science and Information Engineering, 2009 WRI World Congress on
Conference_Location :
Los Angeles, CA
Print_ISBN :
978-0-7695-3507-4
Type :
conf
DOI :
10.1109/CSIE.2009.905
Filename :
5171289
Link To Document :
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