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Rablbauer, Development, microstructure and properties of advanced high-strength and supraductile light-weight steels based on Fe-Mn-Al-Si-(C), Proceedings of the 6th International Conference on Processing and Manufacturing of Advanced Materials, Thermec’2009, Berlin, 2009, 162
Borek, Hot-rolling of advanced high-manganese C-Mn-Si-Al steels, Materials Science Forum 706/709 (2012) 2053-2058
Borek, Hot-Working Behaviour of Advanced High-Manganese C-Mn-Si-Al Steels, Materials Science Forum 654-656 (2010) 266-269
Borek, Hot deformation and recrystallization of advanced high-manganese austenitic TWIP steels, Journal of Achievements in Materials and Manufacturing Engineering 46 (1) (2011) 71-78
Chin, New trends in advanced high strength steel developments for automotive application, Materials Science Forum 638-642 (2010) 136-141

Study on the Compression Properties of Epoxy Matrix Composites Reinforced by PES Warp-knitted Spacer Fabric Fulei Huo1,a, Guoli Zhang1,b, Jialu Li1,c, Guangwei Chen1,d, li Chen1,e 1 Key Laboratory for Advanced Textile Composites of Ministry of Education, Tianjin Polytechnic University, Tianjin 300160, China ahuofulei@163.com, bguolizhang@tjpu.edu.cn, clijialu@tjpu.edu.cn, dchenguangwei@tjpu.edu.cn, echenli@tjpu.edu.cn Keywords: Composites, Spacer fabric, compression, compressive resilience Abstract.
Forum Vol. 250 (2010), p. 1078 [4] M.V.
Jeelani: Materials Science and Engineering.
Forum Vol. 445–446 (2007), p. 54 [5] C.R.
Forum Vol. 29 (2010), p. 793

Product's Optimum Design Based on the Combination of Reverse Engineering and Finite Element Analysis Suyang Li1, a, Siyuan Cheng2,b and Canhua Qiu3,c 1 Faculty of Electro-mechanical Engineering, Guangdong University of Technology, Guangzhou, China 2 Faculty of Electro-mechanical Engineering, Guangdong University of Technology, Guangzhou, China 3 Dishwashing Appliances Division, Midea Living Appliances Group, Foshan, Guangdong Province, China alisuy@gdut.edu.cn, bimdesign@gdut.edu.cn, csdqch@163.com Keywords: Optimum Design, Reverse Engineering, Finite Element Analysis, CAD modeling Abstract.
Therefore, it has played a promising role in the product development cycle and provides a new way of innovation based on the digest and absorption of domestic and foreign advanced manufacturing technology [2-4].
The integration of reverse engineering technology and finite element method aims to improve and innovate in design based on the digest and absorption of domestic and foreign advanced designs so that it will increase the competitiveness in the market.
References [1] Yin Zhongwei: Precision Engineering Vol. 28(2004), p. 293-301
Mori: Materials Forum Vol. 29 (2005), p. 166-171

Introduction Aircraft structure design always developing with the adoption of advanced materials.
Advanced composite material has several advantages such as low density, high strength, high stiffness, and its mechanical property can be designed to fit the demand.
Aircraft structure using advanced composite materials can be lighter than traditional metal structure of 23%-30%[1].
Advanced composite material also has its disadvantage.
The most widely used advanced composite materials such as CFRP, GFRP have their shortage on impact resistance and residual compressive strength.

In Section 3, the conservation time advance mechanism and optimistic time advance mechanism are compared.
In the RTI, federate can not advance logical time by its own, it must promote time advance request clearly, after receiving permission from RTI can the time be advanced.
Before time was advanced to permitted time tg, the rollback manager will execute the following operations: (1) Search the federate state queue to find out state S1 that meet the condition of .
IEEE Standard for Modeling and Simulation (M&S) High Level Architecture (HLA)-IEEE Std 1516TM-2000, 1516.1TM-2000, 1516.2TM-2000, New York: Institute of Electrical and Electronics Engineers, Inc., 2000
[8] High Level Architecture Commercial off the Shelf Simulation Package Interoperation Forum, HLA-CSPIF.

Numerical Simulation of Fatigue Life on MSC.Fatigue and ABAQUS Zhang Jiea，Gu Xiangb ,Ye Haiwei and Li Kangwen Advanced Forming Technology Institute，Jiangsu University, Zhenjiang 212013, China zhangjie_ujs@163.com gohand@163.com Keyword: Laser Shock Processing 7050 aluminum alloy Fatigue life Pull-pull test Abstract.
Table 1 Parameters of laser shock processing Power (GW/cm2) Pulse period (ns) Spot diameter (cm2) Pulse energy (J) 2.91 20 0.09 12 Fatigue test is performed in School of Mechanical and Power Engineering, East China University of Science and Technology.
Xuan: Materials Science and Engineering.
Pergamon 0020-7403(95)00064-X [6] Du, Hai-Ming; Zhou, Xun; Yu and Xiao-Li: Neiranji Gongcheng/Chinese Internal Combustion Engine Engineering, Forum Vol.30(2009), p. 48 [7] José André Marin de Camargo, Herman Jacobus Cornelis: Surface & Coatings Technology.
Forum Vol.201(2007), p. 9448 [8] M.

Preface   Romanian International Conference on Chemistry and Chemical Engineering (RICCCE) is a well known scientific event of the Romanian and foreign chemistry scientists and in this year 2009 the important Meeting comes to its 16 edition.
The aim of RICCCE16 is to provide a forum for presentation and discussion on the main scientific achievements in chemistry and chemical engineering fields and to establish contacts between scientists and companies involved in research, development and production activities.
The Proceedings encloses a selection of 20 papers which will be published in the periodical Key Engineering Materials.
All contributions are peer-reviewed and the volume can serve as a tool for future studies regarding applied aspects of the synthesis and characterization, processing and applications of advanced engineering materials.
President of the Romanian International Conference on Chemistry and Chemical Engineering Prof.

As a new kind of advanced polymer, polyaniline has great potential applications in the technically because its unique doped mechanism, ease of synthesis, stability in aqueous bases and high temperature resistant, et al.
Forum Vol. 63 (1994), p. 47 [4] M.
Forum Vol. 26 (1993), p. 7245 [5] J.
Forum Vol. 58 (1998), p. 7774 [6] Y.
Forum Vol. 48 (1992), p. 91 [7] D.

Low Cycle Fatigue Behavior of Superalloy GH4169 in High Temperature Gas Environment Xin Ding1,a, Dawei Huang1,b*, Xiaojun Yan1,2,3,4,c 1School of Energy and Power Engineering, Beihang University, Beijing 100191, China 2Collaborative Innovation Center of Advanced Aero-Engine, Beijing 100191, China 3National Key Laboratory of Science and Technology on Aero-Engine, Aero-thermodynamics, Beijing 100191, China 4Beijing Key Laboratory of Aero-Engine Structure and Strength, Beijing 100191, China adingxin1015@buaa.edu.cn, bhuangdawei@buaa.edu.cn, cyanxiaojun@buaa.edu.cn Keywords: Low Cycle Fatigue (LCF); High temperature gas (HTG) environment; Hot corrosion Abstract.
Forum Vol.51(2013), pp.68-73
Forum Vol.117(2018), pp.13-20
Forum Vol.46(2014),pp.608-612
Forum Vol.19(2009),pp.77-89

Materials Science Forum Vols. *** (2004) pp.770-774 online at http://scientific.net  2004 Trans Tech Publications, Switzerland Method of Product Development Process Analysis and Reengineering for Concurrent Engineering D.Z.
Zhong 2,c 1 College of Mechanical Engineering, Shandong University, Jinan 250061, P.
China 2 College of Mechanical and Electronic Engineering, Shandong University of Science and Technology, Taian 271019, P.
Wiegand: The Knowledge Engineering Review Vol. 13 (1998), P. 161 [3] J.B.
Wang: Product Development Process in Concurrent Engineering (Tsinghua Univer. 2000) [4] K.S.