Les Inscriptions à la Bibliothèque sont ouvertes en
ligne via le site: https://biblio.enp.edu.dz
Les Réinscriptions se font à :
• La Bibliothèque Annexe pour les étudiants en
2ème Année CPST
• La Bibliothèque Centrale pour les étudiants en Spécialités
A partir de cette page vous pouvez :
Retourner au premier écran avec les recherches... |
Détail de l'auteur
Auteur Heung Soo Kim
Documents disponibles écrits par cet auteur
Affiner la rechercheFree - edge interlaminar stress analysis of composite laminates using interface modeling / Heung Soo Kim in Journal of engineering mechanics, Vol. 138 N° 8 (Août 2012)
[article]
in Journal of engineering mechanics > Vol. 138 N° 8 (Août 2012) . - pp.973–983.
Titre : Free - edge interlaminar stress analysis of composite laminates using interface modeling Type de document : texte imprimé Auteurs : Heung Soo Kim, Auteur ; Jaehun Lee, Auteur ; Maenghyo Cho, Auteur Année de publication : 2012 Article en page(s) : pp.973–983. Note générale : Mécanique aplliquée Langues : Anglais (eng) Mots-clés : Free-edge Interlaminar stress Interface modeling Composite laminates Stress function Résumé : Interlaminar stresses near free edges in composite laminates were analyzed by considering interface modeling. Previous regular analytical solutions for free edge stress are not rigorous in their linear elastic modeling with dissimilar interfaces between homogeneous plies of laminated composites. Singular stress is not practical in reality at the free edge because it nearly never occurs in real situations. Until now, the analytical nonsingular approximate solutions have been accepted even though they cannot show the rigorous singular behavior at the free edges; this shortcoming is corrected within linear elasticity dissimilar interface modeling. In this study, a regular analytical solution is provided, which is rigorous within the linear elastic model featuring smoothly varying material properties through the thickness of the laminates. This interface modeling provides not only nonsingular stresses but concentrated finite interlaminar stresses using the principle of complementary virtual work and the stresses that satisfy the traction-free conditions not only at the free edges but also at the top and bottom surfaces of laminates are obtained. Significant reductions in stresses at the free edge were observed compared with the results without interface modeling. Various stress analyses were performed and the results demonstrate the usefulness of the proposed interface modeling. ISSN : 0733-9399 En ligne : http://ascelibrary.org/doi/abs/10.1061/%28ASCE%29EM.1943-7889.0000399 [article] Free - edge interlaminar stress analysis of composite laminates using interface modeling [texte imprimé] / Heung Soo Kim, Auteur ; Jaehun Lee, Auteur ; Maenghyo Cho, Auteur . - 2012 . - pp.973–983.
Mécanique aplliquée
Langues : Anglais (eng)
in Journal of engineering mechanics > Vol. 138 N° 8 (Août 2012) . - pp.973–983.
Mots-clés : Free-edge Interlaminar stress Interface modeling Composite laminates Stress function Résumé : Interlaminar stresses near free edges in composite laminates were analyzed by considering interface modeling. Previous regular analytical solutions for free edge stress are not rigorous in their linear elastic modeling with dissimilar interfaces between homogeneous plies of laminated composites. Singular stress is not practical in reality at the free edge because it nearly never occurs in real situations. Until now, the analytical nonsingular approximate solutions have been accepted even though they cannot show the rigorous singular behavior at the free edges; this shortcoming is corrected within linear elasticity dissimilar interface modeling. In this study, a regular analytical solution is provided, which is rigorous within the linear elastic model featuring smoothly varying material properties through the thickness of the laminates. This interface modeling provides not only nonsingular stresses but concentrated finite interlaminar stresses using the principle of complementary virtual work and the stresses that satisfy the traction-free conditions not only at the free edges but also at the top and bottom surfaces of laminates are obtained. Significant reductions in stresses at the free edge were observed compared with the results without interface modeling. Various stress analyses were performed and the results demonstrate the usefulness of the proposed interface modeling. ISSN : 0733-9399 En ligne : http://ascelibrary.org/doi/abs/10.1061/%28ASCE%29EM.1943-7889.0000399