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Experiment Material.
Specimens are made by standard 2A12 alloy material with the thickness of 2mm.
Acknowledgements It is a project supported by the National Nature Science Foundation of China (50975284) and Nature Science Foundation of Shanxi Province (SJ08E107).
Department of Defense (2009) [2] MIL-STD-1530C, aircraft structure integrity program, US Air Force (2005) [3] Brooks CL, Prost-Domasky S, Honeycutt K: Corrosion is a structure and economic problem: transforming metrics to a life prediction method (Nato Research and Technology Organization Meeting Proceedings 18, Greece 1998) [4] Goswami TK, Hoeppner DW: Pitting corrosion fatigue of structural materials (Structural integrity in aging aircraft, New York 1995) [5] Ali Merati: International Journal of Fatigue Vol. 27 (2005), p.33 [6] Amilcar Quispitupa, Basir Shafiq, O Marcelo Suarez et al: Journal of Aircraft Vol.43 (2006), p.787 [7] Chen Yueliang, in: Naval aircraft structure corrosion control and strength evaluation (National Defense Industry Press, China 2009) [8] Liu Wenting, Li Yuhai, in: Aircraft Structure Calendar Life Evolution Technology (Aeronautic Industry Press, China 2004) [9] He Yuting :Journal of Air Force Engineering University Vol.6 (2005), p.4 [10] He Yuting, Fan
:Journal of Air Force Engineering University Vol.6 (2006), p.1 [11] He Yuting.: Engineering Science Vol.6 (2006), p.23

Since the basis of modern materials science is multicomponent systems, on their basis it is possible to create various combinations of phases in structural materials with a set of specified properties.
Vasiukov, Concrete and fiber concrete impact strength, Materials Science Forum, 1006 (2020) 101-106
Kovalov, About need of calculations for the steel framework building in temperature influences conditions, IOP Conference Series: Materials Science and Engineering, 708 (1) 012065 (2019)
Shvedun, Experiment Planning for Prospective Use of Barium-Containing Alumina Cement for Refractory Concrete Making, In Materials Science Forum.
Myrgorod, Thermodynamics of solid-phase exchange reactions limiting the subsolidus structure of the system MgO-Al2O3-FeO-TiO2, In Materials Science Forum.

Li: Journal of Materials Chemistry 21(2011), p. 3664
Hu: Journal of Hazardous Materials 171(2009), p. 459
Li: Journal of Hazardous Materials 179(2010), p. 251
Xu: Journal of Materials Chemistry 21(2011), p. 1218
Gu: Journal of Materials Chemistry 20(2010), p. 5110

Materials and method Materials.
Journal of Applied Polymer Science, 96(2), (2005). 557-569
Journal of Applied Polymer Science, 115(2), (2010). 756-776
Chuangchote, On the electrospinning of poly(vinyl alcohol) nanofiber materials: a revisit, 108(2) (2008). 969–978
Journal of Polymer Science Part A: Polymer Chemistry, 42(24) (2004). 6331–6339

Overview of EDM: Prior State of Art Basically Electric Discharge Machining (EDM) is a process for eroding and removing material by transient action of electric sparks on electrically conductive materials.
[4] Kumar, S., Singh, T.P. (2007), “A comparative study of the performance of different EDM electrode materials in two dielectric media”, (IE) (I) Journal-PR, Vol. 8, PP. 3-8
[10] Singh, H., Garg, R., (2009), “Effects of process parameters on material removal rate in WEDM”, Journal of Achievement in Materials and Manufacturing Engineering, Vol. 32, No. 1, pp. 70-74
[11] Pradhan, M.K., Biswas, C.K., (2009), “Modeling and analysis of process parameters on surface roughness in EDM of AISI D2 tool steel by RSM approach”, International Journal of Engineering and Applied Sciences, Vol. 5, No. 5, pp. 346-351
[12] Asif Iqbal, A.K.M., Ahsan Ali khan (2010), “Modeling and analysis of MRR, EWR and surface roughness in EDM milling through Response Surface Methodology”, American Journal of Engineering and Applied Science, Vol. 3,No. 4, pp. 611-619

Being regarded as most ideal materials for automotive applications, solid state hydrogen storage materials should have large gravimetric, large volumetric storage capacity, suitable thermodynamic properties and fast hydrogen sorption and desorption kinetics [1,2].
It is remarkable that the hydrogen storage materials with suitable additives show improved dehydrogenation properties compared with the additives-free materials.
Zhu: Materials today, Vol. 11(2008), p. 36-43
Majzoub: Journal of Materials Chemistry A, Vol. 1(2013), p. 3926-3931
Udovic, et al.: Chemistry of Materials, Vol. 20(2008), p.1245-1247

It states the necessity of the application of composite material solidifying deformation simulation technology in airplane structure’s manufacture. 1 Introduction Composite materials are wildly used in modern large-scale civil use airliner airframe structure, for its advantages of reliable performance, high strength, and entirety modeling structure etc.
According to statistics, in airbus and Boeing related models, the used weight of composite materials occupies more than 50% of that of whole airframe structure, which means that composite materials have become the main structure materials of modern large-scale civil airliner.
But how to control the deformations during the processes of composite material structures’ manufacture is a challenging issue. 2 Solidifying Deformation Mechanism Analysis Composite material solidifying is a solidifying temperature dropping process with nonlinear inner heat source to low thermal conductivity and anisotropic materials.
The aviation science research project MAAXIMUS on composite material was proposed by European Union Seventh Framework, mainly focusing on virtual simulation platform’s construction of airplane’s manufacture processing, and proceeding the virtual simulation calculation before the manufacture of composite material structure.
Journal of Textile Research, 2010(1): 42-45

St 50-2 steel was used as the substrate material, since it is one of the main structural materials used in various fields of technology.
Weiss, Understanding material behaviour of ultrafine-grained aluminium nano-composite sheets with emphasis on stretch and bending deformation, Journal of Materials Processing Technology. 293 (2021) 117082
Materials Science Forum. 938 (2018) 46–53
Krishan, Composite materials: Science and engineering, Springer Science & Business Media, New York, 2013
Caraviello, A numerical/experimental study on the induction heating of adhesives for composite materials bonding, Materials Today Communications. 15 (2018) 203–213

Analysis of aerodynamics behavior of FGM cylindrical panel Li.Yanga, Yuxin.Hao College of Mechanical Engineering, Beijing Information Science and Technology University, Beijing 100192, China, ayangli9087@sohu.com Keywords: Cylindrical panel; functionally graded materials; aerodynamics Abstract.
Introduction Functionally graded materials (FGM) have a smooth and continuous variation of material properties from one surface to another.
Materials properties of the constituents are graded in the thickness direction according to a power-law distribution.
Al-Ajmi, Thermal Buckling and Nonlinear Flutter Behavior of Functionally Graded Material Panels, Journal of Aircraft., 44(5) (2007) 1610–1618
Mohammed, Thermal Buckling and Nonlinear Flutter Behavior of Functionally Graded Material Panels, Journal of Aircraft, 44(5) (2007) 1610–1618

In recent decades, with the development of functional materials, more and more micro-positioning platform are actuated by the physical or chemical effects of functional materials [3].
Closed magnetic circuit mainly consists of GMM rod and cylinder which is made by magnetic material DT4.
Acknowledgements The works was supported by the National Natural Science Foundation of China (Grant No. 50865008), China Postdoctoral Science Fund (Grant No. 20080431005) and Youth Science Fund of Jiangxi province office of education of China (Grant No.GJJ09611).
Sun: Science in China Series E, Vol. 52 (2009) No.7, pp.1858-1865
Lu: Journal of Nanchang Institute of Technology, Vol.27 (2008) No.6, pp.1-5.