Numerical estimation of the mass gain between double symmetric and single bonded composite repairs in aircraft structures

Materials and Design

Volumn 31, Issue 6, 2010, Pages 3073-3077

  Bachir Bouiadjra, B ^a,b   Achour, T ^a   Berrahou, M ^a   Ouinas, D ^c   Feaugas, X ^d  

^a UNIVERSITY OF SIDI BEL ABBES   (Algeria)

^b KING SAUD UNIVERSITY   (Saudi Arabia)

^c UNIVERSITY OF MOSTAGANEM   (Algeria)

^d UNIVERSITÉ DE LA ROCHELLE   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVE PROPERTIES; AIRCRAFT STRUCTURE; BONDED COMPOSITE REPAIRS; COMPOSITE REPAIR; MASS GAIN; NUMERICAL ESTIMATION; SINGLE PATCH; STRESS ABSORPTION; THREE-DIMENSIONAL FINITE ELEMENT METHOD;

AIRCRAFT MANUFACTURE; AIRFRAMES; CRACK TIPS; STRESS INTENSITY FACTORS;

REPAIR;

EID: 77149141397     PISSN: 02641275     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.matdes.2010.01.006     Document Type: Article

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