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Online since: December 2012
Authors: Chiravoot Pechyen, J. Piwsawang, T. Jinkarn
The PP/Co-PP exhibited lower yield strength and young’s modulus, and higher elongation at break than talc composites (data not show here).
Copolymer polypropylene tends to have better stress crack resistance and lower temperature toughness than homopolymer at the expense of slight reductions in other properties.
Copolymer polypropylene tends to have better stress crack resistance and lower temperature toughness than homopolymer at the expense of slight reductions in other properties.
Online since: August 2013
Authors: Li Yan, Ji Shou Zhao
The cyanide leaching reaction mechanism is also discussed.The data at different cyanide concentrations, different temperature and different oxygen pressure are obtained.
The dissolution mechanism involves an electrochemical process in which the anodic reaction is palladium oxidation while the cathodic reaction is oxygen reduction.
The dissolution mechanism involves an electrochemical process in which the anodic reaction is palladium oxidation while the cathodic reaction is oxygen reduction.
Online since: August 2019
Authors: Andi Mu'nisa, A. Muflihunna, Rahmawati Rahmawati, Mamat Pratama, Astuti Astuti, Tenri Ayu Adri
Based on data analysis, the average value of the three antioxidant activity of the replication was 2.482 mg QE / g Extract on the skin of ginger bud fruit and 99.846 mgQE / g extract for lontar fruit skin.
Antioxidants are compounds capable of donating a single electron or hydrogen atom for reduction(8).
Antioxidants are compounds capable of donating a single electron or hydrogen atom for reduction(8).
Online since: May 2004
Authors: Fernando M.B. Marques, A.P. Viskup, E.N. Naumovich, Jorge R. Frade, Vladislav V. Kharton, Alrksey A. Yaremchenko, A.L. Shaula, J.R. Casanova, Ivan P. Marozau
The inset shows the partial ionic,
electron-hole and n-type
electronic conductivities at 1223
K, calculated by fitting of the
experimental data to Eq.(9)
All data on the oxygen permeability presented in this paper corresponds to the membrane feed-side oxygen partial pressure (p2) equal to 21 kPa (atmospheric air).
Low-p(O2) stability limits of (Sr2Fe3)1-x(SrCo)xOz, La0.3Sr0.7Fe1-xAl0.3Cr0.1O3-δ and SrFe0.7Al0.3O3-δ ceramics estimated from the data on total conductivity.
Data on CoO [37], FexO [37] and LaFeO3-δ [8,38] are shown for comparison.
The XRD data showed that dual-phase (Sr2Fe3)1-x(SrCo)xOz ceramics can be obtained for compositions with similar fractions of the components (Table 2).
All data on the oxygen permeability presented in this paper corresponds to the membrane feed-side oxygen partial pressure (p2) equal to 21 kPa (atmospheric air).
Low-p(O2) stability limits of (Sr2Fe3)1-x(SrCo)xOz, La0.3Sr0.7Fe1-xAl0.3Cr0.1O3-δ and SrFe0.7Al0.3O3-δ ceramics estimated from the data on total conductivity.
Data on CoO [37], FexO [37] and LaFeO3-δ [8,38] are shown for comparison.
The XRD data showed that dual-phase (Sr2Fe3)1-x(SrCo)xOz ceramics can be obtained for compositions with similar fractions of the components (Table 2).
Online since: March 2011
Authors: Imed Zaghbani, M. Lamraoui, V. Songmene, M. Thomas, M. El Badaoui
The proposed criterion and method were validated using data obtained during high speed robotic machining of 7075-T6 blocks.
Introduction The robotic machining is one of the emerging technologies for cost reduction in manufacturing processes.
Introduction The robotic machining is one of the emerging technologies for cost reduction in manufacturing processes.
Online since: January 2019
Authors: Daniele Ugues, Mario Rosso, Federico Simone Gobber
The derived data were compared to the experimental investigation of cracks and craters as provided by cycling with a correlation with the surface finishing level of samples.
Lubricants contribute to the reduction of damages due to chemical affinity between the aluminum alloy and the steel constituting the die.
Lubricants contribute to the reduction of damages due to chemical affinity between the aluminum alloy and the steel constituting the die.
Online since: March 2014
Authors: Dietmar Eifler, Marek Smaga, Andreas Sorich
The changes in the physical data were interpreted via microstructural changes observed by scanning- and transmission-electron-microscopy as well as by x-ray investigations.
Chemical composition in weight-% C Cr Ni Nb Ti Mn Mo N Cu Si P S V 0.04 17.60 10.64 0.62 0.02 1.83 0.29 0.007 0.06 0.41 0.02 0.007 0.07 As expected the tensile strength, ultimate strain and reduction in area decrease with increasing temperature (see Tab. 2).
Chemical composition in weight-% C Cr Ni Nb Ti Mn Mo N Cu Si P S V 0.04 17.60 10.64 0.62 0.02 1.83 0.29 0.007 0.06 0.41 0.02 0.007 0.07 As expected the tensile strength, ultimate strain and reduction in area decrease with increasing temperature (see Tab. 2).
Online since: December 2023
Authors: Andreas H. Foitzik, Andrea Böhme, Torsten Döhler, Mandy Hofmann, Jens Neumann, Reinhard Bochem, Ute Geißler
Process data was obtained through electrochemical simulations and subsequently applied to a specially designed micro-galvanic setup.
As the distance increased, the expected homogenization of field lines and reduction of gradual coating effects occurred.
As the distance increased, the expected homogenization of field lines and reduction of gradual coating effects occurred.
Online since: February 2014
Authors: Jian Xiong, Jun Ye, Wen Hao Li
The zero shear viscosity(η0) was obtained by using the Cross model to fit experimental data.
The wide range of CMC applications involves flocculation, detergents, textiles drag reduction, foods, drugs, paper and oil well drilling operation [1].
The wide range of CMC applications involves flocculation, detergents, textiles drag reduction, foods, drugs, paper and oil well drilling operation [1].
Online since: January 2012
Authors: Wisnoe Wirachman, Firdaus Mohamad, Rizal E M Nasir, Wahyu Kuntjoro
The study has been carried out using Computational Fluid Dynamics to obtain aerodynamics data with respect to various sideslip angles (b).
The absence of vertical tail in a BWB aircraft contributes to the reduction of its total drag.
The absence of vertical tail in a BWB aircraft contributes to the reduction of its total drag.