Boundary element analysis of cracked panels repaired by mechanically fastened composite patches

By Widagdo D.   Aliabadi M.H.  

Engineering Analysis with Boundary Elements, Vol. 25, Iss. 4, 2001-04 ,pp. : 339-345

Elsevier

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The application of the dual boundary element method to the analysis of cracked stiffened panels

By Ortiz F.   Los Arcos J.M.   Salgado N.K.   Aliabadi M.H.  

Engineering Fracture Mechanics, Vol. 54, Iss. 1, 1996-05 ,pp. : 91-105

Elsevier

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Fatigue analysis of cracked thick aluminum plate bonded with composite patches

By Tsai G.-C.   Shen S.B.  

Composite Structures, Vol. 64, Iss. 1, 2004-04 ,pp. : 79-90

Elsevier

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Structural Health Monitoring of Cracked Aircraft Panels Repaired with Bonded Patches Using Fiber Bragg Grating Sensors

By Sekine Hideki   Fujimoto Shin-Etsu   Okabe Tomonaga   Takeda Nobuo   Yokobori Toshimitsu  

Applied Composite Materials, Vol. 13, Iss. 2, 2006-03 ,pp. : 87-98

Springer Publishing Company

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Boundary element formulations for the dynamic analysis of cracked structures

By Fedelinski P.   Aliabadi M.H.   Rooke D.P.  

Engineering Analysis with Boundary Elements, Vol. 17, Iss. 1, 1996-01 ,pp. : 45-56

Elsevier

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