Sentence examples for composites start to from inspiring English sources

The TPD curves [9] show that both composites start to decompose at around 170 °C, which is 10 and 55 °C lower than the decomposition temperature of the as-milled AlNaH4 and AlNa3H6, respectively.

Isothermal frequency sweeps on the composites show that storage modulus of PLA-Tannin composites starts to degrade at 15 wt% filler concentration and damping rises.

The interfacial shear strength of the flax/unsaturated polyester composite started to drop sharply at 70% RH and ended up with a more than sixfold reduction at 90% RH.

Temperature programmed desorption (TPD) analyses show that the 2LiBH4 MgH2@CS composite starts to slowly release hydrogen at about 150 °C, which is 245 °C lower than that of the pure 2LiBH4 MgH2; the final hydrogen desorption capacity reaches 9.3 wt% (LiBH4 with a weight loss of 7.0 wt%).

In the field of dental restoration and regeneration, sol-gel silica-based bioactive composites have started to emerge in various applications including coatings, scaffolds and dental tissue regeneration.

Nearly for a decade composites have started to be used more widely in large commercial jet airliners for the fuselage, wing as well as other structural components in place of aluminium alloys due their high specific properties, reduced weight, fatigue performance and corrosion resistance.

The electrical conductivity of the composite films starts to increase if the AgNPs loading on the polymer particle surface is above 20wt.-%wt.-%

In addition, the attitude of the civil engineering industry generally was against the materials but in the late 1980s, composite materials started to have their first major successes in the field of flexural and shear strengthening and seismic retrofitting of degraded concrete structures.

Additionally, PLGA/1.5 % DOX and PLGA/1.5%DOX@2@2 % CNTs composite nanofibers started to have apparent cytotoxicity only at DOX concentration of 25 μg/mL or above.

A novel Selective Laser Melting (SLM) process was applied to prepare bulk-form TiC/Ti5Si3 in-situ composites starting from Ti/SiC powder system.

The idea for using light-weight carbon fiber and epoxy composites started in 1967 with Rolls-Royce but was unsuccessful due to high structural requirements for the aircraft engine.