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ELECTRODEPOSITED NANOCRYSTALLINE Ni-Fe WITH BANDED STRUCTURE Uta Klement1,a, Mehrdad Shahabi-Navid1,b, Glenn Hibbard2,c 1Materials and Manufacturing Technology, Chalmers University of Technology, SE-412 96 Gothenburg, Sweden 2Materials Science & Engineering, University of Toronto, 184 College Street, Toronto, Ontario, M5S 3E4Canada Email: auta.klement@chalmers.se; bmehsha@student.chalmers.se; cglenn.hibbard@utoronto.ca Keywords: Ni-Fe, nanocrystalline material, electroplating, banded structure, EBSD, texture Abstract.
Introduction Electrodeposition is an advanced synthesis method for making nanocrystalline materials.
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Balogh3,g 1 Department of Materials Science and Engineering, Norwegian University of Science and Technology (NTNU), Alfred Getz vei 2b, 7491 Trondheim, Norway 2 Institute of Physics of Advanced Materials, Ufa State Aviation Technical University, 12 K.
Forum Vol. 584-586 (2008), p.528 [7] N.Q.
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Ortiz1. 1 Department of mechanical engineering, DIMEI, National Autonomous University of Mexico, Circuito Exterior de Ciudad Universitaria, Coyoacán, D.F.
At low strains, the driving force for recrystallisation is insufficient and subgrain boundaries cannot break free from the obstacles, resulting in advanced recovery instead of recrystallisation.
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Spin Alignment Studies on the Muon-Site Determination in La2CuO4 Muhammad Redo Ramadhan1,2,3,a, Irwan Ramli1,3,4,b, Dita Puspita Sari5,1,c, Budhy Kurniawan2,d*, Azwar Manaf2,e*, Mohamed Ismail Mohamed-Ibrahim6,f, Shukri Sulaiman6,7,g and Isao Watanabe1,2,3,6,7,h 1Meson Science Laboratory, RIKEN Nishina Center, 2-1 Hirosawa, Wako 351-0198, Japan, 2Department of Physics, Faculty of Mathematics and Natural Sciences, Universitas Indonesia, Depok 16424, Indonesia, 3Muon Spin Resonance Laboratory, Department Condensed Matter Physics, Graduate School of Science, Hokkaido University, Sapporo 060-8010, Japan, 4Department of Physics, Faculty of Science, Universitas Cokroaminoto Palopo, Palopo 91921, Indonesia, 5Department of Regional Environment Systems, Graduate School of Engineering and Science, Shibaura Institute of Technology, Saitama City, Saitama 337-8570, Japan, 6Computational Chemistry and Physics Laboratory, School of Distance Education, Universiti Sains Malaysia, 11800, Malaysia
Acknowledgement The authors gratefully acknowledge the supports from the International Program Associate (IPA) RIKEN, Japan and also for the allocation of computing resources on the Big Wave HOKUSAI Massive Parallel Computer (Project number G19007) from the RIKEN Advanced Center for Computing and Communication (ACCC).
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Lou College of Mechatronics and Control Engineering, Shenzhen University, Guangdong Shenzhen, 518060，P.R.China; susanlou121@163.com Keywords: Rough Set Theory(RST); AZ31 magnesium alloy; 3DFEM simulation; Quantitative; Extrusion.
Introduction As one kind of the lightest engineering materials, magnesium alloys have a great potential for wide application in the automotive industry due to their high strength-to-gravity ratios[1].
Acknowledgement This work is partially supported by Guangdong Provincial Natural Science Foundation of China #9451806001002350 and Research Fund of Shenzhen Key Laboratory of Advanced Mould Manufacturing Technology # MKL09008.
References [1] LI N Y.: Material science forum Vol.488-489(2005),p.931 [2] LI Luo-xing, ZHOU Jie, DUSZCZYK J.: J Mater Process Tech Vol.172(2006),p. 3372 [3] LI Luoxing, LOU Yan: The Chinese Journal of Nonferrous Metals Vol.18(2008 s1), p.252 [4] ZHOU Chi, RUAN Feng: Journal of Plasticity Engineering Vol.14(2007),p.130 [5] YIN Jilong, LI Dayong, PENG Yinhong: Journal of Shanghai Jiaotong University Vol.38 (2004),p.1356 [6] Charlotte Bean, Chandra Kambhampati: International Journal Automation and Computing Vol.1 (2008), p.90 [7] YANG Xinhua, DENG Wu, ZHAO Wenzhong: Journal of Machine Design Vol.24(2007),p.17 [8] Yeong Minkim, Chee Kyeongkim, Jae Cheollee: Advances in Engineering Soft ware Vol.40 (2009),p.202 Fig.4 Grain size at 300℃、400℃ and different strain rate Fig.5 Grain size at 0.03s-1、0.3s-1 、3s-1、90s-1 and different

Qin, Study of the effects of wing sweep on the aerodynamic performance of a blended wing body aircraft, Journal of Aerospace Engineering 221 Part G (2008.). 47 – 55 [2] R.H.
[5] James Chung, Eric Hallberg, Steven Cox, Michael Plyle, Landing Pitch Control Analysis for a Blended Wing Body UCAV, presented at the 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition Orlando World Center Marriott Orlando, Florida, (2010)
[8] Nor Fazira Reduan , Wirachman Wisnoe, Wahyu Kuntjoro , Rizal Effendy Mohd Nasir , Firdaus Mohamad, Zurriati M.A., Study of Aerodynamics Characteristic of BWB Baseline-II, presented at the International Conference on Advances in Mechanical Engineering (ICAME), Selangor,Malaysia, (2010)
Nasir, Zurriati M.Ali, Fazira Reduan, Experiment Results of UiTM’s Blended Wing Body (BWB) Baseline-II UAV using Low Speed Wind Tunnel, presented at the International Conference on Advances in Mechanical Engineering (ICAME), Selangor,Malaysia.,(2010)
[12] Zurriati Mohd Ali, Wahyu Kuntjoro,Wirachman Wisnoe, Rizal E.M Nasir, The Effect of Canard on Aerodynamics of Blended Wing Body, Applied Mechanics and Materials, Mechanical and Aerospace Engineering 110-116 (2011), 4156-4160.

Advanced industry pays great attention to surface hardening technology development.
Scheffler: Hardening technology and wear durability increase for steel 12Cr18Ni10Ti, Proceedings - 2012 7th International Forum on Strategic Technology, IFOST 2012, vol.
Scheffler: Influence of regimes electrolytic plasma cementation on the mechanical properties of steel 12Cr18Ni10Ti, Key Engineering Materials vol. 531-532, 2013, pp. 173-177. http://www.scientific.net/KEM.531-532.173
Naltaev: Changes of mechanical properties of steel 12Cr18Ni10Ti after electrolytic-plasma cementation, Advanced Materials Research, vol. 601, 2013, pp. 59-63. http://www.scientific.net/AMR.601.59 [6] S.А.Kusmanov, I.G.Dyakov, P.N.Belkin: Increase of efficiency of electrochemical-thermal cementation by the modification of the composition of the electrolyte, Tempered materials and coatings, Works of the 8-th all-Russia with international particip.ation of the scientific-technical conference.

Zhang 1 1 State key lab of advanced technology for materials synthesis and processing, Wuhan University of Technology, Wuhan 430070, P.R.China 2 School of science, Wuhan University of Technology, Wuhan 430070, P.R.China a meijuanli@hotmail.com, bCorresponding author: lmzhang@whut.edu.cn Keywords: AlN/BN nano-composite.
Experimental Procedure The initial AlN powder (Fujian Sinocera Advanced Materials Co.
Cho, et al: Key Engineering Materials, Vol. 264-268(2004), p. 873 [4] Y.
Kim, et al: Materials Science Forum Vol.439(2003), p. 131 [10] D.M.

Mechanical Properties and Biocompatibility of Porous Titanium Prepared by Powder Sintering Ik-Hyun Oh 1,a, Hyeon-Taek Son 1,b Chang-Seok Kang1,c , Jae-Seol Lee1,d , Jae-Ik Cho 1,e, Jung-Chan Bae1,f, Byong-Taek Lee2,g and Ho-Yeon Song3,h 1 Gwangju Research Center, Korea Institute of Industrial Technology (KITECH), Gwangju, 506-824, South Korea 2 School of Advanced Materials Engineering, Kongju National University, Chungnam, 314-701, South Korea 3 Department of Microbiology , Soonchunhyang University, Cheonan-city, 366-1, South Korea a ihoh@kitech.re.kr, bsht50@kitech.re.kr, ccskang7@kitech.re.kr, d jslee7@kitech.re.kr, e uwjaeik@kitech.re.kr, fjcbae@kitech.re.kr, glbt@kongju.ac.kr, and h songmic@sch.ac.kr Keywords: porous titanium, spark plasma sintering, porosity, young's modulus, biocompatibility Abstract.
Acknowledgements This research was supported by 2005 research program for infrastructure construction of advanced components and materials from Gwangju-city, Korea References [1] B.
Ndop: Mater Sci Forum Vol. 308 (1999), p. 374

Dimensional Variation of Aluminum Honeycomb Panel on Circular Cutting with Abrasive Jet Machining Technology BULEA Horatiu 1,a *, PAUNESCU Rodica 1,b and FILIP Alexandru Catalin 1,c 1Manufacturing Engineering Department, Transilvania University of Brasov, Eroilor bd. 29, 500036, Brasov ROMANIA a bulea@unitbv.ro, b r.paun@unitbv.ro, c filipal@unitbv.ro Keywords: aluminum honeycomb panel, circular cutting in abrasive jet, dimensional variation of cut diameters.
Diameters results at entrance, at middle and at exit of material Run of the Experimental Tests The experiments were realized in the laboratory of Advanced Technologies, using a waterjet machine type Maxiem, with 20HP and a maximum power of 50,000.00 psi.
Yagüe Fabra, Comparison of Diameter and Area Change Based Methods for Evaluating Break-IN and Break-OUT Damages in Dry Drilled Holes of Aeronautical Carbon Fiber Composites, Materials Science Forum,Volume 797 pag.32-35 4010.4028/www.scientific.net/MSF.797.35
Abdel-Rahman, An Abrasive Waterjet Model for Cutting Ceramics, Proceedings of the International Conference on Mathematical Models for Engineering Science, Puerto de la Cruz, Tenerife, WSEAS Press, 2010
Bulea, Roughness variation and deviation from the perpendicularity of high concentrated ceramic alumium oxide on linear cutting in abrasive jet machining technology, Advances in Production, Automation and Transportation Systems,Proceedings of the 6th International Conference on Manufacturing Engineering, Quality and Production Systems (MEQAPS '13), Brasov, Romania June 1-3, ISSN: 2227-4588,ISBN: 978-1-61804-193-7, WSEAS Press 2013.