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Refinado por: data de publicação: 1997Até2009 remover Nome da Publicação: Composite Structures remover
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1
Compression-after impact behavior of laminated composite plates subjected to low velocity impact in high temperatures
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Compression-after impact behavior of laminated composite plates subjected to low velocity impact in high temperatures

Aktaş, Mehmet ; Karakuzu, Ramazan ; Arman, Yusuf

Composite structures, 2009-06, Vol.89 (1), p.77-82 [Periódico revisado por pares]

Kidlington: Elsevier Ltd

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2
Compressive residual strength at low temperatures of composite laminates subjected to low-velocity impacts
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Compressive residual strength at low temperatures of composite laminates subjected to low-velocity impacts

Sánchez-Sáez, S. ; Barbero, E. ; Navarro, C.

Composite structures, 2008-10, Vol.85 (3), p.226-232 [Periódico revisado por pares]

Oxford: Elsevier Ltd

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3
Core crush criterion to determine the strength of sandwich composite structures subjected to compression after impact
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Core crush criterion to determine the strength of sandwich composite structures subjected to compression after impact

Castanié, Bruno ; Aminanda, Yulfian ; Bouvet, Christophe ; Barrau, Jean-Jacques

Composite structures, 2008-11, Vol.86 (1), p.243-250 [Periódico revisado por pares]

Oxford: Elsevier Ltd

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4
Impact properties of laminated composites with stitching fibers
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Impact properties of laminated composites with stitching fibers

Byun, Joon-Hyung ; Song, Sung-Wook ; Lee, Chang-Hoon ; Um, Moon-Kwang ; Hwang, Byung-Sun

Composite structures, 2006-10, Vol.76 (1), p.21-27 [Periódico revisado por pares]

Oxford: Elsevier Ltd

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5
Damage tolerance of composite toecap
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Damage tolerance of composite toecap

Lee, Seung Min ; Lim, Tae Seong ; Lee, Dai Gil

Composite structures, 2005-02, Vol.67 (2), p.167-174 [Periódico revisado por pares]

Oxford: Elsevier Ltd

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6
Impact damage prediction and failure analysis of heavily loaded, blade-stiffened composite wing panels
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Impact damage prediction and failure analysis of heavily loaded, blade-stiffened composite wing panels

Wiggenraad, J.F.M ; Zhang, X ; Davies, G.A.O

Composite structures, 1999-06, Vol.45 (2), p.81-103 [Periódico revisado por pares]

Oxford: Elsevier Ltd

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7
An engineering approach for predicting residual strength of carbon/epoxy laminates after impact and hygrothermal cycling
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An engineering approach for predicting residual strength of carbon/epoxy laminates after impact and hygrothermal cycling

Qi, B. ; Herszberg, I.

Composite structures, 1999-12, Vol.47 (1), p.483-490 [Periódico revisado por pares]

Oxford: Elsevier Ltd

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8
Impact resistance and tolerance of interleaved tape laminates
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Impact resistance and tolerance of interleaved tape laminates

Duarte, Andre ; Herszberg, Israel ; Paton, Rowan

Composite structures, 1999-12, Vol.47 (1), p.753-758 [Periódico revisado por pares]

Oxford: Elsevier Ltd

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9
Composite steel–CFRP SHS tubes under axial impact
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Composite steel–CFRP SHS tubes under axial impact

Bambach, M.R. ; Elchalakani, M. ; Zhao, X.L.

Composite structures, 2009-02, Vol.87 (3), p.282-292 [Periódico revisado por pares]

Kidlington: Elsevier Ltd

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10
On the response of thin-walled CFRP composite tubular components subjected to static and dynamic axial compressive loading: experimental
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On the response of thin-walled CFRP composite tubular components subjected to static and dynamic axial compressive loading: experimental

Mamalis, A.G. ; Manolakos, D.E. ; Ioannidis, M.B. ; Papapostolou, D.P.

Composite structures, 2005-08, Vol.69 (4), p.407-420 [Periódico revisado por pares]

Oxford: Elsevier Ltd

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