Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Vinay Damodaran"'
Publikováno v:
Materials & Design, Vol 212, Iss , Pp 110268- (2021)
In this paper, we propose a novel design and fabrication strategy to produce architected structures for use as the core in composite sandwich structures. A traditional foam core or honeycomb structure is lightweight and stiff, but susceptible to perm
Externí odkaz:
https://doaj.org/article/ee3de2f574de4d0b8197b8007a6959d7
Publikováno v:
American Society for Composites 2021.
The long-term goal of this ONR funded project is to facilitate the design of architected composites that play a key role in damage tolerant and resilient structures. The main emphasis is on developing new composite structures with improved performanc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7be67975abb104d617dccb3c65dc6e37
https://doi.org/10.12783/asc36/35869
https://doi.org/10.12783/asc36/35869
Autor:
Kiran Shahapurkar, Mrityunjay Doddamani, Vinay Damodaran, P Breunig, Sunil Waddar, Pavana Prabhakar, P. Jeyaraj
Publikováno v:
Journal of Composite Materials. 54:535-547
Sandwich composites and syntactic foams independently have been used in many engineering applications. However, there has been minimal effort towards taking advantage of the weight saving ability of syntactic foams in the cores of sandwich composites
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f17206030cd0634ee6b4adc01e94f72
https://doi.org/10.1177/0021998319885000
https://doi.org/10.1177/0021998319885000
Publikováno v:
American Society for Composites 2020.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3feca0f0515b571b33688fc77878ac0b
https://doi.org/10.12783/asc35/34850
https://doi.org/10.12783/asc35/34850
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::43b36adeffcdfb2ca29a7092ae58fe31
https://doi.org/10.2514/6.2020-1926
https://doi.org/10.2514/6.2020-1926
Publikováno v:
Materials & Design, Vol 157, Iss, Pp 60-73 (2018)
Delamination is a common failure mode observed in fiber reinforced polymeric composites subjected to thermo-mechanical loads. Reinforcements at the interlaminar regions or in the through-thickness direction have been previously shown to improve the d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5ac6c585ce696e941c85c9e8f5397127
https://doi.org/10.1016/j.matdes.2018.07.006
https://doi.org/10.1016/j.matdes.2018.07.006
Publikováno v:
American Society for Composites 2019.
Composite sandwich structures, while offering desirable mechanical properties such as light weight, high flexural rigidity and energy dissipation under loading, also suffer from inelastic damage accumulation under loading conditions. With a greater d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::be23100264f58fc417bd00f2f2afc5be
https://doi.org/10.12783/asc34/31404
https://doi.org/10.12783/asc34/31404
Publikováno v:
Scopus-Elsevier
Fiber reinforced ceramic matrix composites (FRCMCs) have been shown to retain exceptional thermal and mechanical properties at high temperatures in inert atmosphere. However, FRCMCs like carbon fiber reinforced carbon ceramic matrix composites (C/C C
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1d0e9412291b54b9214079d0f5a52e05
https://doi.org/10.12783/asc34/31308
https://doi.org/10.12783/asc34/31308
Publikováno v:
Journal of Composites Science
Volume 5
Issue 1
Journal of Composites Science, Vol 5, Iss 27, p 27 (2021)
Volume 5
Issue 1
Journal of Composites Science, Vol 5, Iss 27, p 27 (2021)
Adhesive bonding is increasingly being used for composite structures, especially in aerospace and automotive industries. One common joint configuration used to test adhesive strength is the single-lap shear joint, which has been widely studied and sh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6cb172c5910dfaad993a513a01016e3c
https://doi.org/10.3390/jcs5010027
https://doi.org/10.3390/jcs5010027
Autor:
Vinay Damodaran, Pavana Prabhakar
Publikováno v:
Scopus-Elsevier
Delamination is a common failure mode observed in fiber reinforced polymeric composites when subjected to various thermo-mechanical loads. Additional reinforcements at the interlaminar regions or in the through-thickness direction have shown to impro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8c2eb108f65dcb08bc4f7b2907287499
https://doi.org/10.12783/asc2017/15206
https://doi.org/10.12783/asc2017/15206