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The data of each classification were noted before the next classification.
Therefore, coefficient decreases with the reduction of temperature compression.

The lattice parameters of the material were calculated by MDI.Jade.5.0 soft, the lattice constants of the simple are: a=10.310Å, b= 6.001Å, c= 4.687Å, that is very close to the standard LiFePO4 data.
The uniform distribution of the carbon and appropriate reduction of the particle size can significantly improved the diffusion rate and the conductivity of the LiFePO4/C [6].

Image capture Image processing Image storage Start End Y N Input of image Image pre-processing Garbo feature extraction  PCA dimension reduction extraction  ELM classification Fig.6.
The interface consists of image data, motion control, monitoring control, spray cleaning process control, etc.

Adaptive Immune Vaccine Algorithm Adaptive immune vaccine algorithm [9] can effectively overcome disadvantages of the basic genetic algorithm, like premature convergence, poor ability of local search, and diversity reduction.
Characteristic data are shown in Table 1.

Fig. 4b shows broadening diffraction peaks of the porous film, which implies a reduction in crystalline size.
The barrier height () and the ideality factor (n) can be determined from the y-intercept and the slope of the fitted curve, respectively, by using a linear curve fit to the forward characteristics of ln(I) against the V data.

In addition, there are reduction factor exist: when rock and tunnel has an angle of 10 to 20 degrees, the factor is 0.8, and hence for IV category rocks, it can only withstand 1.6 to 0.45 MPa of pressure.
Now, the slope of those three pitshafts are 22, 25, 25 degree separately, and according to drilling data the angle of drilling is 17~18 degrees.

Under the arid climate, both dry and little wet saline soils have melt sinking features, which will be melt sinking deformation and got strength reduction under the soils’ weight pressure or supplementary pressure of the earth surface [4].
Table.2 Data of loading tests Ground treatment methods Test category Test Plate Final Final Number area settlement load (m²) (mm) (kPa) Determined by the relative deformation Deformation modulus (MPa) Allowed settlement (mm) Bearing capacity (kPa) Gravel pile Single pile 5 0.196 38.04 600 20 402.89 17.51 The soil between the piles 2 0.196 42.48 400 7.5 120.05 5.21 Single pile composite foundation 5 1.96 33.79 300 24 233.35 10.32 DCR Gravel pier 2 0.785 41.05 600 15 539.21 23.38 The soil between the piers 2 0.785 44.30 600 15 262.63

However, further reduction of these large epitaxial defects is required in order for SiC devices to handle higher power densities.
With respect to the data in Table 1, 27 sites where TSDs existed with the morphological feature were checked, and it was confirmed that extended defects appeared in 21 sites.

Table 1 Basic parameters of the engine Items Value Items Value Cylinder diameter/cm 10.2 Cooling way Liquid cooling Stroke/cm 10.1 the exhaust valve opens 102（ATDC） Cylinder number 4 the exhaust valve fully opens 40（BBDC） Compression ratio 16.5：1 the exhaust valve opens 115（ATDC） Fuel Diesel or jet A1 the exhaust valve fully opens 36（BBDC） Enter the main data of each part and the related physical parameters, the whole engine model is showed as fig1 Fig.1 The GT-POWER model of one type of piston aviation oil engine Change the air inlet conditions when the altitude reaches 5000 meters where air pressure and temperature declines, the temperature was 254K, temperature pressure was 50.545KPa Simulations show that the air compress efficiency decreases. from 100% to 30% when works at high altitude from sea level to 5000 meters.
Numerical Investigation of Turbo lag Reduction in HD CNG Engines by Means of Exhaust Valve Variable Actuation and Spark Timing Control[M].International Journal of Automotive Technology, 2010(3):289-306 [4] Ding Xianfei, Xu Bin.

In this study, among other changes of body posture, the reduction of the hip angle was most obviously, reaching 136.5°.
The data showed that He had quite high flight height and, therefore, long flight time which was 0.78s.