Results 61 to 70 of about 570,927 (212)
e-PolymersThis article aims to evaluate the effects of mesh size change on the mechanical properties of GFRP laminates, via low-velocity impact and compression-after-impact (CAI) test, and the failure mechanism was analyzed. Through vacuum-assisted resin infusion,
Huang Hongyuan +6 more
doaj +1 more source
Fatigue Performance of Composite Laminates After Low-velocity Impact
Cailiao gongcheng, 2016 Compression-compression fatigue tests were carried out on T300/5405 composite laminates after low-velocity impact, compression performance of the laminates with different impact damages was studied together with its fatigue life and damage propagation ...
LIANG Xiao-lin, XU Xi-wu, LIN Zhi-yu
doaj +1 more source
Cailiao gongcheng, 2017 The low-velocity impact and compression after impact (CAI) properties of three-dimensional (3D) five-directional carbon fiber/epoxy resin braided composites were experimentally investigated.
YAN Shi +4 more
doaj +1 more source
Properties of three graphite/toughened resin composites [PDF]
Results are presented from an experimental evaluation of IM7/977-2, IM7/F655, and T800/F3900. Data presented include ply-level (unidirectional laminate) strength and moduli, unnotched and notched (open hole) tension and compression properties of quasi ...
Dow, Marvin B., Smith, Donald L.
core +1 more source
, 2017 Today's HPC applications are producing extremely large amounts of data, such that data storage and analysis are becoming more challenging for scientific research.
Cappello, Franck +3 more
core +1 more source
A portable load cell for in-situ ore impact breakage testing [PDF]
, 2002 This paper discusses the design and characterisation of a short, and hence portable impact load cell for in-situ quantification of ore breakage properties under impact loading conditions.
Banini, George, Bourgeois, Florent
core +1 more source
Properties of two composite materials made of toughened epoxy resin and high-strain graphite fiber [PDF]
Results are presented from an experimental evaluation of IM7/8551-7 and IM6/18081, two new toughened epoxy resin, high strain graphite fiber composite materials.
Dow, Marvin B., Smith, Donald L.
core +1 more source
Experimental analysis of impact and post-impact behaviour of inserts in Carbon sandwich structures [PDF]
, 2019 In aeronautics, honeycomb sandwich structures are widely used for secondary structures such as landing gear doors, flaps or floors, and for primary structures in helicopters or business jets.
Bouvet, Christophe +5 more
core +3 more sources
Experimental study on impact and flexural behaviors of CFRP/aluminum-honeycomb sandwich panel
e-PolymersTo investigate the impact and flexure behavior of carbon fiber reinforced polymers/aluminum-honeycomb sandwich panel, low-velocity impact, compression-after-impact (CAI), and three-point flexure tests are conducted carefully.
Zhao Shicheng +5 more
doaj +1 more source
Structure of shock compressed model basaltic glass: Insights from O K-edge X-ray Raman scattering and high-resolution ^(27)Al NMR spectroscopy [PDF]
, 2012 The detailed atomic structures of shock compressed basaltic glasses are not well understood. Here, we explore the structures of shock compressed silicate glass with a diopside–anorthite eutectic composition (Di_(64)An_(36)), a common Fe-free model ...
Asimow, Paul D. +7 more
core +1 more source