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Al-Saadoun, S.
Al-Gahtani, Effect of tricalcium aluminate content of cement on corrosion of reinforcing steel in concrete, Cem.
El-Mohr, T.D.

After that,samples were placed in the plant chamber system specified to Malaysian local climate control with a relative humidity (RH) of 80% and 300C temperature for 14 days according to Harrison et al.[9].
[9] T.A.Harrison, et al., Experience of Using the prTS 12390-12 Accelerated Carbonation Test to Assess the Relative Performance of Concrete.
El-Sayad, and I.G.

Until recently, Wang X-S et al. [8] and Diederich et al. [9]reported the synthesis of 1,1-dicyanobuta-1,3-diene derivatives. but as far as we know, no condensation renactions with sarcosine or proline as catalyst have been reported.
Elemental analysis of the compound was performed on an Elementar Vario EL (Germany) instrument.

Researches have indicated that damping behaviour of Mg varies with large number of factors, such as solute element, grain size and its distribution, grain boundary condition, texture, and et al.
Abed El-Al: J.

The contact to p-type base is made by firing an Al containing paste that produces a local high doping of Al, thus over compensating the shallow emitter diffusion.
Spiegel, et al.: Solar Energy Materials & Solar Cells, Vol. 91, 2007, p. 1638
Ostendorf, et al.: Appl.
El-Tahchi, A.
Zhang, et al.: Physica B, Vol. 355, 2005, p. 408.

El (GPa) Et (GPa) Gtl (GPa) 21.6 21.6 4.66 0.18 Three different methods have been performed to calculate the Mode I fracture toughness according to ASTM standards: the Compliance Calibration (CC), the Modified Compliance Calibration (MCC) and the Modified Beam Theory (MBT).
As comparison, Mouritz et al. [12] has studied several types of reinforcement (stitched, 3D, 2D textiles) and showed that laminates with 2D reinforcement with and without stitching have identical values of GIi.
Mouritz et al. [12] report that the interlaminar toughness is an increasing function of the density of stitching.
For example, Guenon et al. [15] found that the GIc of a 3D woven carbon/epoxy composite is nearly 15 times higher than a classical 2D carbon/epoxy laminate.
Several authors already suggested values for the penalty parameter as Zou et al. [24].

Nordine, et al., Composites Science and Technology 51 193 (1994)
[3] El-Giar, E.
Bridges, et al., Electrochemical Society, 147(2) 586 (2000)
Jiang, et al., Micro-electroplating of Nickel on Copper Substrate , Hsin-Chu, Taiwan, (1998)
Chang, et al., Fabrication of Copper Columns by MAGE Process , Nantou, Taiwan, (2004)

Emission peak located at about 418 nm was observed in ZnO thin film or Cr-doped ZnO nanoparticles in the literatures [26-27]; emission peak at about 496 nm (2.5 eV) was discerned in ZnO thin film or Al-doped ZnO thin film [27-29].
Ding et al. proposed that the violet peak 410 nm originated from the electron transition from the bottom of conduction band to the shallow acceptor level formed by Zn vacancies[29]，while Wei et al. proposed that peak at 405nm has been attributed to transition from oxygen-vacancy related shallow donor level to valence peak[30].
Wei et al. considered that the emission at 486 nm might be caused by the electronic transition from the conduction band to acceptor level of OZn[27], while Ding et al. ascribed the luminescence centered 492 nm to the electron transition from the recombination of singly ionized oxygen vacancy (VO) electron transition from Zn interstitial to Zn vacancies[29, 31].
Pal et al. indicated that the emission at pump excited holes in the valence band [32].
El-Shaer, A.

Mehleri et al.
Visa et al., RO patent 125253 A2 (2008)
Visa et al., RO patent 126335-A0 (2010)
Visa et al., RO patent 126149 A0 (2010)
Visa et al., RO patent 126230 (2010)

Low cycle fatigue experiments were carried out by Samuel et al. [6] at elevated temperatures and Siva et al. [7], Paul et al. [8] at ambient temperature.
Hong et al. [9] and Huang et al. [10] have studied a metallurgical aspect of dynamic strain aging (DSA).
This is attributed to dynamic strain aging (DSA) phenomena due to that UTS increases and %El and %RA decreases.
Samuel et al. [6] have shown that with the increase in temperature fatigue life increases up to 250oC and a further increase in temperature fatigue life goes on decreasing.
But however, according to Huang et al. [10] and Lee and Kim [13], DSA induced hardness leads to an increase in fatigue life despite the loss of ductility.