Numerical analysis of the patch shape effects on the performances of bonded composite repair in aircraft structures

2012 ◽  
Vol 43 (2) ◽  
pp. 391-397 ◽  
Author(s):  
Mhamdia Rachid ◽  
B. Serier ◽  
B. Bachir Bouiadjra ◽  
M. Belhouari
Keyword(s):  
Numerical Analysis ◽  
Composite Repair ◽  
Aircraft Structures ◽  
Patch Shape ◽  
Bonded Composite ◽  
Shape Effects

Numerical analysis of the performances of bonded composite repair with two adhesive bands in aircraft structures

2008 ◽  
Vol 82 (1) ◽  
pp. 84-89 ◽  
Author(s):  
H. Fekirini ◽  
B. Bachir Bouiadjra ◽  
M. Belhouari ◽  
B. Boutabout ◽  
B. Serier
Keyword(s):  
Numerical Analysis ◽  
Composite Repair ◽  
Aircraft Structures ◽  
Bonded Composite

Optimisation of the sizes of bonded composite repair in aircraft structures

2012 ◽  
Vol 41 ◽  
pp. 171-176 ◽  
Author(s):  
S.M. Fekih ◽  
A. Albedah ◽  
F. Benyahia ◽  
M. Belhouari ◽  
B. Bachir Bouiadjra ◽  
...  
Keyword(s):  
Composite Repair ◽  
Aircraft Structures ◽  
Bonded Composite

Elastic plastic analysis of bonded composite repair in cracked aircraft structures

2010 ◽  
Vol 30 (1) ◽  
pp. 66-72 ◽  
Author(s):  
A. Albedah ◽  
B. Bachir Bouiadjra ◽  
W. Ouddad ◽  
M. Es-saheb ◽  
F. Binyahia
Keyword(s):  
Composite Repair ◽  
Aircraft Structures ◽  
Elastic Plastic ◽  
Plastic Analysis ◽  
Bonded Composite

scholarly journals Elliptical and circular bonded composite repair under mechanical and thermal loading in aircraft structures

2014 ◽  
Vol 17 (5) ◽  
pp. 1219-1225 ◽  
Author(s):  
Faycal Benyahia ◽  
Abdulmohsen Albedah ◽  
Bel Abbes Bachir Bouiadjra
Keyword(s):  
Thermal Loading ◽  
Composite Repair ◽  
Aircraft Structures ◽  
Bonded Composite

Experiments Method Design Applied to Optimization of Patch Repairs for Cracked Plates

2013 ◽  
Vol 577-578 ◽  
pp. 441-444
Author(s):  
M. Belhouari ◽  
S.M. Fekih ◽  
K. Madani ◽  
A. Amiri ◽  
Bel Abbès Bachir Bouiadjra
Keyword(s):  
Design Method ◽  
Three Dimensional ◽  
Aircraft Structures ◽  
Patch Shape ◽  
Cracked Plates ◽  
Repair Efficiency ◽  
Experimental Design Method ◽  
Bonded Composite ◽  
Patch Repairs ◽  
Integral Variation

The optimization of the patch shape of bonded composite repair in aircraft structures is an efficient way to improve the repair performance. In this study the three-dimensional nonlinear finite element method is used to determine the J integral variation along the front of repaired crack with bonded composite patch in aircraft structures. The experimental design method was applied to optimize the patch shape and size in order to determine the most influencing dimension on the repair efficiency.

Analysis of the adhesive failure in bonded composite repair of aircraft structures using modified damage zone theory

2013 ◽  
Vol 50 ◽  
pp. 433-439 ◽  
Author(s):  
M. Fari Bouanani ◽  
F. Benyahia ◽  
A. Albedah ◽  
A. Aid ◽  
B. Bachir Bouiadjra ◽  
...  
Keyword(s):  
Damage Zone ◽  
Adhesive Failure ◽  
Composite Repair ◽  
Aircraft Structures ◽  
Bonded Composite

Analysis of the distribution of thermal residual stresses in bonded composite repair of metallic aircraft structures

2009 ◽  
Vol 46 (4) ◽  
pp. 1023-1027 ◽  
Author(s):  
L. Aminallah ◽  
T. Achour ◽  
B. Bachir Bouiadjra ◽  
B. Serier ◽  
A. Amrouche ◽  
...  
Keyword(s):  
Residual Stresses ◽  
Composite Repair ◽  
Aircraft Structures ◽  
Thermal Residual Stresses ◽  
Bonded Composite
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