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The kinematic geometry of the architecture for the non over-constrained device is shown in Fig.1.
Figure 1.
The displacement of the platform is: (1) Where are the orientation errors around the x, y, z axes and be referred to in the text as Equation (1)
For legs j, k and l (j, k, l = 1, 2, 3, 4, i – j – k – l), the condition for having a maximum of the fourth kind on the interval is that: (1) (2) is orthogonal to X-X0.
Pittens, R.P Podhorodeski, A family of Stewart platforms with optimal dexterity, Journal of Robotics Systems 10 (4) (1993) 463–479

Fig. 1.
Dislocation cell structures in aluminum substrate annealed for 1 h (a), 3 h (b), 6 h (c), 10 h (d) at 300 ºC, for 1 h (e), 3 h (f), 6 h (g), 10 h (h) at 400 ºC, and for 1 h (i), 3 h (j), 6 h (k), 10 h (l) at 500 ºC.
Anodic films formed from annealed aluminum substrate for 1 h (a) and 10 h (b, c) at 300 ºC, for 1 h (d) and 10 h (e, f) at 400 ºC, and for 1 h (g) and 10 h (h, i) at 500 ºC.
References [1] H.
Forum Vol. 475-479 (2005), p. 3919 [5] O.

The schematic of the hybrid structure is shown in Fig.1.
The total composite wall is named as substructure 1, and the total shear wall is named as substructure 2.
According to Timoshenko beam theory [5] (Timoshenko 1990), the relation equations among the shear deformation, the flexural deformation and external horizontal loads of substructure 1 are introduced as （1） （2） To substructure 2, the relation equation between the flexural deformation and external horizontal loads is introduced as （3） where G1A1 and E1I1 is the shear stiffness and the flexural stiffness of the substructure 1; E2I2 is the flexural stiffness of the substructure 2; q(x) is the interaction between substructure 1 and substructure 2.
Combining Eq. (1) with Eq. (11), yq1 can be derived as （11） Based on the prior assumption, yb2=yb1+yq1, and y=yb2.
Mech., 36(4), 463-479 [2] Yao, Q.F., Hou L.N. and Huang, W. (2008), “Shear capacity of multi-ribbed composite wall”, Proceeding of the tenth International Symposium on Structural Engineering for Young Experts, Changsha, China, October

Table 1: The sample composition in mol% glasses and labeling.
Figure 1.
[1] L.
Yana, Characterization of NiO nanoparticles by anodic arc plasma method, Journal of Alloys and Compounds 479 (2009) 855–858
Solid State Science and Technology 14(1) (2006) 115-120

In high temperature tensile Table 1.
Fig. 1.
References [1] A.A.
Vol. 9(1) (2003), p. 21 [6] Y.J.
Forum Vol. 475-479 (2005), p. 537 [7] M.S.

The sintering process was in the same condition as was adopted above in the procedure 1.
Results and Discussion The microstructure of the sintered ceramics obtained in the procedure 1 was exhibited through SEM photos of the etched surfaces (Fig. 1).
The grains coalesced further to form a homogeneous integrated microstructure with a few pores and interfaces among grains in the 5% (Fig 1-c) and 7% (Fig 1-d) LiCl-doped ceramics.
References [1] H.
Feng, etc., Materials Science Forum Vol. 475-479(2005), p.2367-2370 [12] R.

Fig.1 explains the definition of SI schematically.
The stress states at failure are summarized in Table 1.
The maximum value of SI equals to 1 when p'=p'max, and it can be a negative value when the Skempton's pore pressure parameter A >1
References [1] ASTM D4767-11 (2011).
W. (1981), “Consolidation and settlement of soft clay,” Soft Clay Engineering, Elsevier, pp. 479~566

There is an inflection point between stage 1 and 2, at 765 oC.
In this experiment, two X65 samples were prepared, which were heated to 750 oC (in stage 1 of Fig. 2) or 780 oC (just exceeding stage 1 of Fig. 2) at about 200 oC/min, held for 10min and then quenched to water at room temperature.
Therefore, the slope in stage 1 (Fig. 2) is somewhat lower than that in stage 2.
References [1] C.
Lee, Materials Science Forum, (475-479)2005, p.3169-3172

The schematic diagram and real experimental apparatus are shown in Fig. 1 and Fig. 2, respectively.
(2) Where, S is the thread interval (m), υχ is the velocity of x direction (ms-1) , r is the radius of the mold (m), υt is tangential velocity (ms-1), ω is angular velocity(s-1), π is circumference ratio, β is velocity loss rate, which has been gained in 3.2.
Fig. 7 Rotation speed VS width of the thread at time 1.524s 4.
Program number: 2009ZX04014-081 References [1] H.G.Fu, Q.
A Vol. 479 (2008), p. 253–260 [2] J.W.Gao and C.Y.Wang: Mater.

And the two-dimensional histogram is shown in Fig. 1(b).
Equations of L1, L2, L3 and L4 are shown in Eq. 1.
，1/21 (3) ，01/2 (4) Choose Structuring Element.
References [1] REN Y H.
Beijing：Publishing House of Electronics Industry, 2003：474-479 [3] MARAGOS P.