Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Mehran Ghalami-Choobar"'
Autor:
Ehsan Pedram, Hamed Ahmadi, Ali Kabiri, Mehran Ghalami Choobar, Omid Razmkhah, Neil Fellows, Gholamhossein Liaghat
Publikováno v:
Polymer Composites.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6a452bd3c57e8a6b80e149677b931225
https://doi.org/10.1002/pc.27307
https://doi.org/10.1002/pc.27307
Autor:
Gholamhossein Liaghat, Amar Bayat, Ghasem Dehghani Ashkezari, Hadi Sabouri, Mehran Ghalami-Choobar
Publikováno v:
International Journal of Mechanical Sciences. 159:315-324
This paper presents an analytical model for the high-velocity impact behavior of autoclaved aerated concrete (AAC) blocks under flat-ended cylindrical projectile. This model employs an energy balance approach to derive the governing differential equa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ad1158bb842aa81e6bc28e7a06bc5d80
https://doi.org/10.1016/j.ijmecsci.2019.05.043
https://doi.org/10.1016/j.ijmecsci.2019.05.043
Publikováno v:
Composite Structures. 201:315-325
This paper investigates the eccentric low-velocity impact of Fiber metal laminates (FMLs) subjected to spherical projectile using a unified Zig-Zag plate theory. The presented zig-zag plate theory enforces transverse shear stress continuity through t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::abc898638b94953436276466a76292af
https://doi.org/10.1016/j.compstruct.2018.06.027
https://doi.org/10.1016/j.compstruct.2018.06.027
Autor:
Omid Razmkhah, A. Aboutorabi, Hamed Ahmadi, Gholamhossein Liaghat, Mojtaba Sadighi, Mehran Ghalami-Choobar
Publikováno v:
International Journal of Mechanical Sciences. 141:491-501
In the present study, static behavior of short hybrid laminate beams was investigated using a unified zig-zag theory (ZZT) containing various beam theories as special cases. This theory satisfies transverse shear stresses continuity in the interface
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b9194d65f6bfae4b50fc8496acd72d9
https://doi.org/10.1016/j.ijmecsci.2018.04.030
https://doi.org/10.1016/j.ijmecsci.2018.04.030
Publikováno v:
Aerospace Science and Technology. 32:142-152
In this study, the high velocity impact response of sandwich specimens with FML skins and polyurethane foam was investigated by experimental and numerical approaches. Impact tests were performed using a helium gas gun to identify deformation mechanis
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::270e365e5650b46e69a83fb861428289
https://doi.org/10.1016/j.ast.2013.12.005
https://doi.org/10.1016/j.ast.2013.12.005