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Fig. 1.
In the first case, a load which is 10% of the local Load 1 is added to Load 1 in t=40 sec.
References [1] E.
Strbac, "Rotor Flux Magnitude and Angle Control Strategy for Doubly Fed Induction Generators", Wiley Interscience, Wind Energy ,Vol. 9, pp. 479-495, June 2006
Strbac, "Rotor Flux Magnitude and Angle Control Strategy for Doubly Fed Induction Generators", Wiley Interscience, Wind Energy, Vol. 9, pp. 479-495, June 2006

Fig.1.
References [1] Peng Siping, Shen Yan, Lu Xuepeng, etc all.
Radar Science and Technology, Vol. 8 (2010) No.5:474-479
JOURNAL OF GRAPHICS, Vol. 8 (2010) No.5:474-479
Int J Adv Manuf Technol, 2011,(52):1-14

The effect of ageing processes on the toughness and the yield strength of the Li-containing Al-Zn-Mg-Cu alloys (Al-5.6%Zn-1.9%Mg-1.6%Cu-1.1%Li-0.24Cr) was investigated.
Tensile tests were performed at a rate of 1×10 -3 m·s-1.
References [1] M.
Jones: Engineering Materials, vol. 1, (Butterworth Heinemann, Woburn, MA, USA 1996)
Forum Vol. 475-479 (2005), p. 325 [6] T.

In this study, copper, indium, and sulfur (selenium) powders with a molar ratio of 1:1:2.4 were mixed, ball-milled, and then sintered under vacuum at various temperatures.
There are two prominent peaks at 295 cm-1 and 479 cm-1: the peak at 295 cm-1 is attributed to the symmetric A1 modes of typical chalcopyrite CIS units [13], and the peak at 479 cm-1 is ascribed to the CuxS phase in sample B [14].
The plot of sample C presents two additional peaks at 240 cm-1 and 337cm-1, which are attributed to E(3) and E(6) models of the CIS, respectively [15-17], and there is no scattered peaks related to CuxS phase.
These results agree well with the previous XRD analysis (Fig.1 (b)).
References [1] G.P.

FAILURE ANALYSIS OF DIESEL ENGINE INTAKE VALVE Ali GÖKSENLĐ 1, a and Barlas ERYÜREK 1,b 1 Faculty of Mechanical Engineering, Istanbul Technical University, Taksim, Istanbul, Turkey.
Impact ratio coefficient is 1,2.
Considering size factor (kD) as (for diameter 5 mm) kD=0,99 and surface factor (very fine polished) kS= 0,98 [4], the modified endurance limit (σI E) is MPa I E 479=σ .
In this case, fatigue safety factor (υ) can be calculated as; 68,2 179 479 === F I E σ σ υ
References [1] A.

Fig. 1 shows the FTIR spectra of OR-CLAY.
It could be seen that dual kurtosis of Si–O stretching vibration of clay appeared at 1036 cm-1, and bending vibration bands of Si–O and Al–O appeared at 463 cm-1and 521 cm-1.
The second stage weight loss is found to be 2–16 % from 303 °C to 479 °C.
The third stage weight loss begins from 479 °C .
References [1] A.

Introduction People are paying more attention on the loss of wood due to wood defect[1].
T Seen from fig.1, lumbers are hanged by very flexible rubber rope, so lumbers are approximate “free state”.
The second order frequency of lumber containing between 7th and 8th node is 480.04Hz, 479.35Hz is the second order frequency of between 17th and 18th node.
Both 480.04Hz and 479.35Hz is under the second order frequency of standard lumber 481.44Hz.
References [1] Wang Lihai, Yang Xuechun, Xu Kaihong.

When (j=a, b, c) is open, =1; when it is closed, =0.
n=1,2,…,12 (5) (2) Switching Table Table 1 is a new switching table.
References [1] Xu Xiaopin, Huang Jin, Yang Jiaqiang.
IEEE Trans on Industry Applications, 1998, 34, (6): 473-479
IEEE Trans. on Industry Applications, 1998, 34(6): 473-479.

The nominal compositions of the alloy is Al-7%Zn-0.1%Sn-0.015%Ga (in mass per cent).
Fig.1.
References [1] Y H Zhao, L Y Lin, Z C Liu, et al.
Rare Metal Materials and Engineering，2005，34(3) : 479-482
Rare Metal Materials and Engineering，2005，34(3) : 479-482.

Research on wind turbine airfoils aerodynamic performance of trailing edge modification Shang-ke Yuan 1, a, Zi-qin Zhao 1,b 1College of Civil Engineering , Lanzhou Institute of Technology, Lanzhou 730050, China ayuansk@126.com, b122090752@qq.com Keywords: trailing edge.aerodynamic performance.Gurney flap Abstract.
It can be seen in Fig. 1. that the difference in lift coefficient is very small for all airfoils when the angle of attack is lower than 5 deg.
References [1] Peter Fuglsang, Christian Bak.
Forum Vol. 479-487(2003), p.125 [4] STANDISH K J, VAN DAM C P.
Aerodynamic analysis of blunt trailing edge airfoil[J].Journal of solar energy engineering.Forum Vol. 479-487(2003),p.125 [5] Baker J P, Mayda E A, Dam C P Van.