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The experimental approach to this problem that has recently attracted intensive research interest is nanoindentation, due to its flexible and non-destructive materials testing mode and its ability to characterize materials at a very small scale.
Kulkarni, Journal of Crystal Growth, 310, 324 (2008). 7.
Wolf, Semiconductor Science and Technology, 11, 139 (1996). 25.
Voronkov, Journal of Crystal Growth, 59, 625 (1982). 28.
Hartwig, Materials Science and Engineering B, 36, 30 (1996).

Introductions Engineering cementitious composites (ECC) is a new type of composite materials, has been extensively studied and applied in many countries [1].
Wang, Experimental study on the axial compressive strength and elastic modulus of GHPFRCC, Applied Mechanics and Materials.
Keoleian, Design of green engineered cementitious composites for improved sustainability, ACI Materials Journal. 105(2008) 567-575
Luo, Study on the reinforced concrete column strengthened by GHPFRCC with high volume of fly ash, Applied Mechanics and Materials.
Xu, Uniaxial compressive properties of ultra high toughness cementitious composite, Journal of Wuhan University of Technology-Material. 26(2011) 762-769.

Experimental part Materials.
Zaat, A quarter of a century of plasma spraying, Annual Review of Materials Science, 13 (1983), pp. 9-42
Hyland, Bubble formation in NiCr splat on aluminum substrate during plasma spray: Surface chemistry effect, Materials Science and Engineering 4 (2009), No. 1, pp.1-5
Matějíček, Multiple-Approach Evaluation of WSP Coatings Adhesion/Cohesion Strength, Journal of Thermal Spray Technology, Volume 22 (2012), Issue 2-3, pp. 221-232
Gill, Residual stresses in thermal spray coatings and their effect on interfacial adhesion: A review of recent work, Journal of Thermal Spray Technology, 5 (1996), No. 4, pp. 401-418.

It is a technique well suit for joining many hard-to-weld metals without filler materials.
Journal of Materials Processing Technology, 146.2(2004)263-272
Science and Technology of Welding and Joining, 8(2007)634-640
Rare Metal Materials And Engineering, 7(2006) 1172-1176
Materials for Mechanical Engineering, 5(2012) 47-49.

Materials and Methods The material used in this investigation was 30CrMnSiNi2A steel with the following chemical composition: 0.26~0.34 C, 0.9~1.2 Si, 1.0~1.3 Mn, 0.015 S, 0.025 P, 1.4~1.8 Ni, 0.9~1.2 Cr, 0.25 Cu, 0.20 W, 0.15 Mo and the rest Fe (wt %).
The maximum tensile stress would move from material surface into material interior, thus the fatigue cracks would produce in a certain tensile stress area under residual compressive stress layer instead of emerging in material surface.
At this time, because fatigue cracking behaviors of materials were closely related to the dislocation motion kinetics, the dislocation of fatigue source could freely spread at the material surface.
References [1] Hai jun WU, Wei YAO, Feng lei HUANG, Lian sheng ZHANG and Yong jian LI: Transactions of Beijing Institute of Technology Vol. 30 (2010), p. 258 [2] Feng HUAN, Xian min LIU and Chun xu WANG: Journal of Iron and Steel Research Vol. 15 (2003), p. 25 [3] A Javidi, U Rieger and W Eichlseder: International Journal of Fatigue Vol. 30 (2008), p. 2050 [4] Yu kui GAO, Xiang bin LI, Qing xiang YANG and Wei YAO: Materials Letters Vol. 61 (2007), p. 466 [5] K Dalaei and B Karlssona: Materials Science and Engineering A Vol. 528 (2011), p. 7323 [6] S Bagherifard, I F Pariente and R Ghe: Procedia Engineering Vol. 2 (2010), p. 1683 [7] D R Askeland and P P Phule: Essentials of Materials Science and Engineering (Defence Industry Press, Beijing 2004)
[8] T Roland, D Retraint, K Lu and J Lu: Materials Science and Engineering A Vol. 445 (2007), p. 281 [9] Yu kui GAO: Rare Metal Materials and Engineering Vol. 33 (2004), p. 1000

The physical description parameter contains the material characteristics, real constant, and the related parameters of mesh.
The composite rockwool plate cabin material is a new fire proof cabin material widely used all over the world.
Acknowledgements This work was financially supported by the Liaoning provincial Natural Science Foundation (20072144), and the Central university basic scientific research Foundation (2011QN106).
Journal of sound and vibration,1971,14:115-135 [2]LIU Xiao-ming,WANG Xiao-yu,CHEN Ci-hui,Numerical analysis of low and middle frequency noise in ship cabin using fluid-structure coupling[J].Journal of Ship Mechanics,2008,12(5):812-818(In Chinese) [3]Zhou Yuhai,Liu Gang,Hu Wei,Zou Zhewei,Dong Haoming,Divide-integration Method in Parametric Modeling of Jib Structure of Deck Crane Based on APDL[J],Journal of Wuhan University of Technology,2007,31(6):1128-1131(In Chinese) [4]Liugang.Optimal design for thin-walled box beam based on material strength reliability.Journal of Wuhan University of Technology Mater.Sci.Ed.2003,18(1):69 - 71 [5]Mesd D J,Yaman Y.The harmonic response of rectangular sandwich plates with multiple stiffening:A flexural wave analysis[J].J.Sound Vib,1991,145(3):409-428 [6]Jee-Hun Song, Suk-Yoon Hong, Won-Ho Joo Analysis of structure-borne noise in ship cabins using a floating floor with an inserted viscoelastic layer [J].Mar Sci Technol,2009,14:127–135 [7]Tongjun Cho
,Vibro-acoustic characteristics of floating floor system:The influence of frequency-matched resonance on low frequency impact sound [J].journal of Sound and Vibration,2012,332,33-42 [8]YU Da-peng,ZHAO De-you,WANG Yu,Influence of damped material and the ship model of acoustic on the ship cabin noise[J].Journal of Ship Mechanics,2010,14(5):539-548(In Chinese)

A.a, Mohd Zaheruddin K.b, Rahmat A.c,Shamsul B.Jd and Khairel R.Ae School of Materials Engineering, Universiti Malaysia Perlis, Arau Perlis.
Acknowledgement This work was financially supported by the Universiti Malaysia Perlis short term grant (9001-00343) and School of Materials Engineering Universiti Malaysia Perlis.
Journal of Experimental Animal Science, Volume 42, Issue 2, August 2002, Pages 102-112
Journal of Materials Processing Technology, Volume 202, Issues 1–3, 20 June 2008, Pages 536-542
Materials Letters, Volume 76, 1 June 2012, Pages 11-14, ISSN 0167-577X

Preface 2011 International Conference on Chemical, Mechanical and Materials Engineering (CMME 2011) was held in Guangzhou, China, from July 8-10, 2011, serving as a platform for expertise exchange.
CMME 2011 had drawn the attention of researchers from various disciplines: Chemical, Mechanical and Materials engineering, etc.
From which 57 papers have been accepted for presentation at the conference and will be published by TTP, in Advanced Materials Research (AMR) Journal (ISSN: 1022-6680), which is online available in full text via the platform www.scientific.net.
We express our special gratitude to all the members of the General Committee Chairs, Program Committee Chairs, Technical Program Committee and Steering Committee who worked so hard to prepare the conference and who supported the conference so professionally. 2011 International Conference on Chemical, Mechanical and Materials Engineering (CMME2011) is co-sponsored by Maldives College of Higher Education, ACM Hong Kong Chapter and Huazhong University of Science and Technology, China.
Finally, we would like to thanks all the authors, speakers and participants of this conference for taking part in and contributing to the International Conference on Chemical, Mechanical and Materials Engineering.

It should be remembered that Kamal model was initially adapted to describe the slow vulcanization rates of rubber materials [13].
Osswald, Modeling Processing of Silicone Rubber: Liquid Versus Hard Silicone Rubbers, Journal of Applied Polymer Science. 119 (2010) 8
Wriggers, Thermo-mechanical behaviour of rubber materials during vulcanization, International Journal of Solids and Structures. 42 (2005) 4758-4778
Sourour, Kinetics and thermal characterization of thermoset cure, Polymer Engineering & Science. 13 (1973) 59-64
Farid, Techniques used for determining cure kinetics of rubber compounds, European Polymer Journal. 43 (2007) 4783-4799

Under the long-term effect of alternate stress, many machine parts would fracture when their stress is less than strength limit of materials or even less than yield limit stress of that.
First measure the metallic materials fatigue limit, then draw the S-N curve and observe the phenomenon of fatigue failure and fracture characteristics .
The above situation illustrates that the determination of fatigue limit of metallic materials is related to the structure of specify specimen.
By comparing the test data with theoretical value, it can be concluded that fatigue limit of the specify specimen differs from that of materials of specimen.
References: [1] Surenh S: Materials Fatigue (translated by National Defence Industry Press, Beijing, 1993) (In Chinese )