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As identified in wear resistance tests, there are two stages in the behavior of the friction coefficient (Fig. 1).
I II 1 2 3 m Fig. 1.
SEM. 100 µm 20 µm a b 1 2 3 10 µm c d 2.5 µm Fig. 3.
References [1] Deuis R L, Yellup J M and Subramanian C 1998 Composites Science and Technology 58 (2) 299-309
[5] Agarwal A and Dahotre N B 1999 Journal of Materials Engineering and Performance 8(4) 479-486

It is found that the AE signal is an effective parameter for monitoring the texture of machined surface. 1.
Micro V-grooving experiments 2. 1 Experimental setup Micro v-groove machining was performed using a 3-axis micro-stage.
Machining experiment was carried out with a single crystal diamond tool on a machine as shown in Fig. 1.
Table. 1 shows the specifications of the experimental equipment.
Valente, Analysis of tool and workpiece interaction in diamond turing using graphical analysis of acoustic emission, CIRP Annals – Manufacturing Technology, Vol.52, (2003), pp.479-482 [10] X.

Table 1.
Fig. 1.
Fig. 1 shows the high seasonality of demand.
Table 1.
Energy Conversion and Management 50 (2009) 479–489.

Trent and Wright [1] suggest that 99 per cent of the work done is converted into heat.
CET Fig.1.
For the present experiment, in addition to the machining parameters already reported, it was adopted the advance MCFT 1-0.1, speed of 710 rpm and a slice thickness of 3 mm.
Table 1 – Results measured in the process of bleeding of the Al-7wt%Si alloy.
References [1]E.M.

Effect of Material Composition on Mechanical Properties of Ceramics-Metal Composite Materials Tomoyuki FUJII1, a, Keiichiro TOHGO1, b, Hiroyasu ARAKI1, c, Katsunori WAKAZONO2, d, Masaki ISHIKURA 1, e and Yoshinobu SHIMAMURA1, f 1Department of Mechanical Engineering, Shizuoka University, 3-5-1 Johoku, Naka-ku, Hamamatsu, 432-8561, Japan 2INAX Corporation, 5-1 Koiehonmachi, Tokoname, Aichi, 479-8585, Japan attfujii@ipc.shizuoka.ac.jp, btmktoug@ipc.shizuoka.ac.jp, criyo-8888@ka.tnc.ne.jp dfleeting-dream@hotmail.co.jp, emishikura@mechmat.eng.shizuoka.ac.jp, ftysimam@ipc.shizuoka.ac.jp Keywords: Titanium, Partially stabilized zirconia, Composite, Hot pressing method, Powder metallurgy, Hardness, Bending strength, X-ray diffraction Abstract.
Scanning electron microscope (SEM) photographs of these powders are shown in Fig. 1.
The bending stress was calculated by the following equation from the applied load P, sB=3P(L-L0)2bh2 (1) Fig. 1.
References [1] Y.
McCracken: Journal of prosthodontics, Vol. 8, No. 1 (1999), p. 40 [4] K.

Experimental Figure 1 shows the components of a SOFC short stack in the cassette design.
References [1] J.
Shaffer, 2003, Fuel Cells 2003, 3, No. 3, pp. 1-7, (2003)
Boltze, J. of Power Sources, 154, Issue 2, pp. 479-488, (2006)
Schwank, J. of Power Sources, 160, Issue 1, pp. 474-484 (2006)

Their chemical compositions are (in wt.%): 0.15C - 1.5Mn - 1.5Si for steel LC and 0.4C - 1.37Mn - 1.45Si for steel HC.
Figure 1: Microstructure of steel LC water quenched from 750°C after no deformation.
It is known that the martensitic transformation is accompanied by a transformation strain that causes the plastic deformation of the surrounding ferrite grains [1].
References [1] P.J.
A, Vol. 273-275 (1999), pp. 475 - 479 [4] R.

Torre1,5,a 1 European Lab. for Non-Linear Spectroscopy (LENS), Università di Firenze, via Carrara 1, I-50019 Sesto Fiorentino, Italy. 2 Istituto Nazionale di Ottica (INO) - CNR, Largo E.
PU2-MoS2 PU1-MoS2 Figure 1.
In both samples, the concentration of nanoparticles was less than 1 wt-%.
References [1] T.
Self-assembly of subnanometer-diameter single-wall MoS2 Nanotubes, Science, Vol. 292, 2001, pp. 479-481

The chemical compositions and physical properties of slag are given in table 1.
References [1] Erhan guneyisi, Mehmet Gesoglu.
Materials and Structures, 2008, (41) : 479-493
Pozzolanic and cementitious by products as mineral admixtures for concrete-a critical review, vol. 1.
Pozzolanic and cementitious by products in concretes-another look, vol. 1.

The numerical analysis for the turbulence in the 180°bend tube was taken by Patankar etc. [1].
Obviously, when is large, coefficient , and close to 1.
The mesh was shown as Fig.1.
References [1] Patankar, S.V.
TABAKOFF: Journal of Aircraft, Vol.12 (1975) , pp. 471-479