Zobrazeno 11 - 18
of 18
pro vyhledávání: '"Mehrdad N"'
Publikováno v:
Developments and Applications of Advanced Engineering Ceramics and Composites
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0b12e381a94a92f3102e02585fb5fda3
https://doi.org/10.1002/9781118144091.ch15
https://doi.org/10.1002/9781118144091.ch15
Publikováno v:
ASME 2010 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, Volume 2.
In this study, a brittle epoxy resin has successfully been toughened by very small concentrations of SiC and diamond nanoparticles. The tensile stress-strain response (based on the ASTM tensile tests for polymers) and the fracture energy release rate
Publikováno v:
Smart Materials, Adaptive Structures and Intelligent Systems, Volume 1.
In this study, the effects of using aligned multi-walled carbon nanotube (MWCNT) nanofoam films as adhesive reinforcements to enhance the shear strength of composite joints are examined. The MWCNT reinforced adhesive nanofoam films are used to bond c
Publikováno v:
Construction and Building Materials. 4:194-207
Instrumented drop weight impact and compression after impact test methods were used to assess the impact performance and damage tolerance of firm-stacked, woven carbon fibre-reinforced PEEK and woven carbon fibre-reinforced PPS composite systems. The
Publikováno v:
Multifunctional Nanocomposites.
This paper presents activities related to the development of nanocomposites and hierarchical nanocomposites; at the Hawaii Nanotechnology Laboratory of the Department of Mechanical Engineering of the University of Hawaii at Manoa. On nanocomposites,
Publikováno v:
Aerospace.
An analytical micromechanics approach is presented to model the effective longitudinal mechanical properties of Metal-Core Piezoelectric Fibers (MPF). The model assumes general orthotropic material properties for the piezoelectric as well as the core
Publikováno v:
SPIE Proceedings.
This work presents manufacturing and testing of active composite panels (ACPs) with embedded piezoelectric sensors and actuators. The composite material employed here is a plain weave carbon epoxy prepreg fabric with about 0.33 mm ply thickness. The
Publikováno v:
Aerospace.
This work presents manufacturing and testing of active composite panels (ACPs) with embedded piezoelectric sensors and actuators. The composite material employed here is a plain weave carbon/epoxy prepreg fabric with about 0.3 mm ply thickness. A cro
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