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Department of Aeronautics and Space Engineering, Tohoku University, Sendai, Japan
Selected Publications:
Tamate, O. and Sekine, H., “Postbuckling Behavior of Thin Curved Panels Under Axial Compression,” Bulletin of JSME, Vol. 12, No. 51, 1969, pp. 415-420.
Inokuti M, Sekine H, Mura T (1978) General use of the Lagrange multiplier in nonlinear mathematical physics. In: Nemat-Nasser S (ed) Variational method in the mechanics of solids. Pergamon Press, Oxford, pp 156–162
Fukunaga, H., and Sekine, H., “Stiffness Design Method of Symmetric Laminates Using Lamination Parameters,” AIAA Journal, Vol. 30, No. 11, 1992, pp. 2791–2793
H. Fukunaga, H. Sekine, M. Sato, Optimal design of symmetric laminated plates for fundamental frequency, J. Sound Vib., 171 (1994), pp. 219–229
Fukunaga, H. and Sekine, H. “A laminate design for elastic properties of symmetric laminates with extension-shear or bending- twisting coupling”. Journal of Comp. Mat., Vol. 28, No. 8, pp. 708-731, 1994.
H. Fukunaga, H. Sekine, M. Sato, and A. Iino, “Buckling design of symmetrically laminated plates using lamination parameters,” Computers & Structures, vol. 57, no. 4, pp. 643–649, 1995.
H. Sekine, N. Hu, H. Fukunaga, and T. Natsume, “Low-velocity impact response of composite laminates with a delamination,” Mech. Compos. Mater. Struct., vol. 5, pp. 257–278, 1998.
N. Hu, B. Hu, B. Yan, H. Fukunaga, and H. Sekine, “Two kinds of C0-type elements for buckling analysis of thin-walled curved beams,” Computer Methods Applied Mechanics and Engineering, vol. 171, no. 1-2, pp. 87–108, 1999.
Hu, N., Sekine, H., Fukunaga, H., and Yao, Z. H. Impact analysis of composite laminates with multiple delaminations. International Journal of Impact Engineering, 22, 633–648 (1999)
Ning Hu, Hisao Fukunaga, Hideki Sekine, Kouchakzadeh Mohammad Ali, “Compressive buckling of laminates with an embedded delamination”, Composites Science and Technology Vol. 59, 1999, pp. 1247-1260, doi: S0266-3538(98)00166-3
Sekine, H., Hu, N., and Kouchakzadeh, M.A., 2000. Buckling analysis of elliptically delaminated composite laminates with consideration of partial closure of delamination. Journal of Composite Materials 34(7): 551–573.
Diaconu CG, Sato M, Sekine H. Layup optimization of symmetrically laminated thick plates for fundamental frequencies using lamination parameters. Struct Multidisc Optim. 2002;24(4):302–311
C. G. Diaconu, M. Sato, and H. Sekine, “Buckling characteristics and layup optimization of long laminated composite cylindrical shells subjected to combined loads using lamination parameters,” Composite Structures, vol. 58, no. 4, pp. 423–433, Dec. 2002.
Diaconu, C. G., Sato, M., and Sekine, H., “Feasible Region in General Design Space of Lamination Parameters for Laminated Composites,” AIAA Journal, Vol. 40, No. 3, 2002, pp. 559–565
Afsar, A. M., and Sekine, H., 2002, “Inverse Problems of Material Distributions for Prescribed Apparent Toughness In, FGM Coatings Around a Circular Hole in Infinite Elastic Media,” Compos. Sci. Technol., 62, pp. 1063– 1077.
C. G. Diaconu and H. Sekine, “Layup Optimization for Buckling of Laminated Composite Shells with Restricted Layer Angles,” AIAA Journal, vol. 42, no. 10, pp. 2153–2163, Oct. 2004.
H. Sekine, H. Shirahata, and M. Matsuda, Vibration characteristics of composite sandwich plates and layup optimization of their laminated FRP composite faces, Adv. Compos. Mater., vol. 14, pp. 181–197, 2005.
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