SIF for cracks repaired with single composite patch having two adhesive bands and double symmetric one in aircraft structures

Computational Materials Science

Volumn 44, Issue 2, 2008, Pages 542-546

  Bezzerrouki, M ^a   Bouiadjra, B Bachir ^a   Ouinas, D ^b  

^a UNIVERSITY OF SIDI BEL ABBES   (Algeria)

^b UNIVERSITY OF MOSTAGANEM   (Algeria)

Author keywords

Adhesive; Composite patch; Double patch; Ratio; Shear modulus; SIF; Single patch having two adhesive bands; Thickness

Indexed keywords

AIRCRAFT MANUFACTURE; AIRFRAMES; CRACK TIPS; CRACKS; ELASTIC MODULI; FINITE ELEMENT METHOD; MAINTENANCE;

COMPOSITE PATCH; DOUBLE PATCH; RATIO; SHEAR MODULUS; SIF; SINGLE PATCH HAVING TWO ADHESIVE BANDS; THICKNESS;

STRESS INTENSITY FACTORS;

EID: 55849133760     PISSN: 09270256     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.commatsci.2008.04.029     Document Type: Article

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