Stacking sequence optimizations for composite laminates using fractal branch and bound method: Application for supersonic panel flutter problem with buckling load condition

By Hirano Yoshiyasu   Todoroki Akira  

Advanced Composite Materials, Vol. 13, Iss. 2, 2004-06 ,pp. : 89-106

Taylor & Francis Ltd

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An inner approximation method incorporating a branch and bound procedure for optimization over the weakly efficient set

By Yamada S.   Tanino T.   Inuiguchi M.  

European Journal of Operational Research, Vol. 133, Iss. 2, 2001-01 ,pp. : 267-286

Elsevier

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Compressive property degradation of composite stiffened panel due to debonding and delaminations

By Suemasu Hiroshi   Kurihara Keisuke   Arai Keiji   Majima Osamu   Ishikawa Takashi  

Advanced Composite Materials, Vol. 15, Iss. 2, 2006-07 ,pp. : 139-151

Taylor & Francis Ltd

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A branch and bound algorithm for mixed zero-one multiple objective linear programming

By Mavrotas G.   Diakoulaki D.  

European Journal of Operational Research, Vol. 107, Iss. 3, 1998-06 ,pp. : 530-541

Elsevier

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Evaluation of energy release rate for delamination defects at the skin/stringer interface of a stiffened composite panel

By Armentani E.   Caputo F.   Esposito R.   Godono G.  

Engineering Fracture Mechanics, Vol. 71, Iss. 4, 2004-03 ,pp. : 885-895

Elsevier

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