Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Ahmed El Bouhmidi"'
Publikováno v:
Frattura ed Integrità Strutturale, Vol 13, Iss 50, Pp 126-140 (2019)
In this paper the demand for curved stiffened panels composite from carbon fiber reinforced plastics (CFRP) has emerged; these structures are most frequently used in aerospace engineering. Nearly 50% of the primary structure of the Boeing 787 is made
Externí odkaz:
https://doaj.org/article/0bd6a2a3814e44b6a0a064af8470a55e
Publikováno v:
Frattura ed Integrità Strutturale, Vol 13, Iss 50 (2019)
In this paper, gradual demand for curved, stiffened panels composite emerged from carbon fiber reinforced plastics (CFRP); these are structures that are frequently used in aerospace engineering. Up to 50% of the primary structure of the Boeing 787 is
Externí odkaz:
https://doaj.org/article/3dd40cf791e547a984d340ccca3963cc
Autor:
Ahmed El Bouhmidi, Hasnae Boubel, Mohamed Rougui, Abdelmajid Bybi, Omaima Elmrabet, Ouadia Mouhat
Publikováno v:
Solid State Phenomena. 298:161-166
The present work proposes a vibration study with different surface and layers orientations at 0°, 15°, 30°, 45°, 60°, 75° and 90°using the Abaqus finite element code, the frequencies Stratified laminate composite panels were studied and the co
Publikováno v:
Pollack Periodica. 14:169-180
In this research, buckling behavior of rectangular plates of symmetric and antisymmetric laminated composite having centered circular hole under in-plane static loadings is analyzed with t...
Publikováno v:
Frattura ed Integrità Strutturale; Vol 13 No 50 (2019): October 2019; 126-140
Frattura ed Integrità Strutturale; V. 13 N. 50 (2019): October 2019; 126-140
Frattura ed Integrità Strutturale, Vol 13, Iss 50, Pp 126-140 (2019)
Frattura ed Integrità Strutturale, Vol 13, Iss 50 (2019)
Frattura ed Integrità Strutturale; V. 13 N. 50 (2019): October 2019; 126-140
Frattura ed Integrità Strutturale, Vol 13, Iss 50, Pp 126-140 (2019)
Frattura ed Integrità Strutturale, Vol 13, Iss 50 (2019)
In this paper, gradual demand for curved, stiffened panels composite emerged from carbon fiber reinforced plastics (CFRP); these are structures that are frequently used in aerospace engineering. Up to 50% of the primary structure of the Boeing 787 is
Autor:
Ahmed El Bouhmidi, Mohamed Rougui
Publikováno v:
MATEC Web of Conferences, Vol 149, p 02013 (2018)
In this research, buckling behavior of perforated rectangular plate of symmetric and anti-symmetric laminated composite is investigated based on Finite element analysis. The presence of hole may cause redistribution of stresses in plates with reducti