Papers

［Computational Mechanics］
●Analysis of Direct Current Potential Field around Multiple Spherical Defects(109)
      Naoya TADA, Eisuke NAKAYAMA, Takayuki KITAMURA and Ryuichi OHTANI
●Thermal Deformation of a Piezothermoelastic Composite Plate (An Antisymmetric Angle-Ply Laminate Plate)(117)
      Naotake NODA and Shinya KIMURA
［Stress Analysis and Design］
●Real-Coded Adaptive Range Genetic Algorithm and Its Application to Aerodynamic Design(124)
      Akira OYAMA, Shigeru OBAYASHI and Kazuhiro NAKAHASHI
●Optimal Structural Design of Compliant Mechanisms (Considering of Quantitative Displacement Constraint)(130)
      Susumu EJIMA, Shinji NISHIWAKI, Minako SEKIGUCHI and Noboru KIKUCHI
●A Study on Maximization of Dynamic Crushing Energy Absorption of Square Tubes with and without Stiffener(138)
      Jing HAN and Koetsu YAMAZAKI
［Material Evaluation］
●Dynamic Buckling Experiments on Liquid Containing Cantilever Cylindrical Shells under Horizontal Excitation(146)
      Mayumi FUKUYAMA, Masaki NAKAGAWA, Takeshi YASHIRO, Yukihiro TOYODA and Hiroshi AKIYAMA
●Creep Life Prediction of Ni-Base Superalloy Used in Advanced Gas Turbine Blades by Electrochemical Method(156)
      Shin-ichi KOMAZAKI, Tetsuo SHOJI and Minoru SATO
●The Estimation of Temperature Rise in Low-Cycle Fatigue of TiNi Shape-Memory Alloy(166)
      Satoru MIKURIYA, Takafumi NAKAHARA, Hisaaki TOBUSHI and Hideo WATANABE
［Fracture and Fatigue］
●Improvement in Fatigue Strength of Silicon Manganese Steel SUP7 by Using a Cavitating Jet(173)
      Hitoshi SOYAMA
●Evaluation of Dynamic Fracture Toughness of Unidirectional CFRP Laminates(179)
      Tadaharu ADACHI, Masahiro ARAI, Naoki SAKABE and Hiroyuki MATSUMOTO
●Improvement in Static, Impact and Fatigue Properties of CFRP due to CNBR Modification of Epoxy Matrix(186)
      Kenichi TAKEMURA and Toru FUJII
［Discussion］
●Anti-Plane Shear Crack in a Piezoelectric Layer Bonded to Dissimilar Half Spaces(196)
      Fumio NARITA, Yasuhide SHINDO and Koji WATANABE

198　　　Contents of the Transactions of the J.S.M.E.