1 "변형률 보간 9절점 쉘 요소를 이용한 적층복합판 과 쉘의 선형 정적 해석 및 자유진동 해석" 한국 전산구조공학회 16 (16): 32-37, 2004
2 "개선된 고차이론을 이용한 복합재료 적층구조물의 탄성 및 점탄성적 휨, 진동해석" 한국강구조학회 14 (14): 1-12, 2002
3 "XFINAS 3.0" Konkuk University, Korea 2007
4 "The Residual Stress of Functionally Graded Materials" 13 : 1-9, 2001
5 "The Effect of Varying the In-plane Loads and Stacking Sequence on the Vibration Analysis of Composite Stiffened Plates" 2007
6 "The Crack Problem for a Nonhomogeneous Plane" 609-614, 1983
7 "Residual/ thermal Stress in FGM and Laminated Thermal Barrier Coatings" 69 : 145-165, 1995
8 "On Vibration of Functionally Graded Plates according to a Refined Trigonometric Plate Theory" 5 (5): 279-297, 2005
9 "Nonlinear Transient Thermoelastic Analysis of Functionally Graded Ceramicmetal Plates" 4457-4476, 1988
10 "Multiple Cracking in Functionally Graded Ceramic/metal Coatings" 32 : 2853-2871, 1995
1 "변형률 보간 9절점 쉘 요소를 이용한 적층복합판 과 쉘의 선형 정적 해석 및 자유진동 해석" 한국 전산구조공학회 16 (16): 32-37, 2004
2 "개선된 고차이론을 이용한 복합재료 적층구조물의 탄성 및 점탄성적 휨, 진동해석" 한국강구조학회 14 (14): 1-12, 2002
3 "XFINAS 3.0" Konkuk University, Korea 2007
4 "The Residual Stress of Functionally Graded Materials" 13 : 1-9, 2001
5 "The Effect of Varying the In-plane Loads and Stacking Sequence on the Vibration Analysis of Composite Stiffened Plates" 2007
6 "The Crack Problem for a Nonhomogeneous Plane" 609-614, 1983
7 "Residual/ thermal Stress in FGM and Laminated Thermal Barrier Coatings" 69 : 145-165, 1995
8 "On Vibration of Functionally Graded Plates according to a Refined Trigonometric Plate Theory" 5 (5): 279-297, 2005
9 "Nonlinear Transient Thermoelastic Analysis of Functionally Graded Ceramicmetal Plates" 4457-4476, 1988
10 "Multiple Cracking in Functionally Graded Ceramic/metal Coatings" 32 : 2853-2871, 1995
11 "Multi- paradigm Expert System Architecture based upon the Inverse Design Concept International Workshop on Artificial Intell- igence forIndustrial Applications" 1988
12 "Mechanics of composite plates and shells: Theory and Analysis" CRC press, Boca Raton. 2004
13 "Linear Static and Dynamic Analysis of Laminated Composite Plates and Shells using a 4-node Quasi-conforming Shell Element" 37 (37): 237-248, 2006
14 "Free Vibration of Antisymmetric Angle-ply Laminated Plates including Transverse Shear Deformation by the Finite Element Method" 565-576, 1979
15 "Formulation of Quasi-conforming Element and Hu-Washizu Principle" 1 247-2 250, 1984
16 "Exact Solution for Functionally Graded Anisotropic Elastic Composite Laminates" 37 (37): 1903-1920, 2003
17 "Cracking in Sigmoid Functionally Graded Coating" 18 : 41-53, 2002
18 "Buckling of Rectangular Plates with Mixed Edge Supports" 14 : 401-416, 2002
19 "Buckling Analysis of Variable Curvature Panels and Shells" 43 : 321-329, 1999
20 "Analytical solutions for free vibration of laminated composite and sandwich plates based on a higher-order refined theory" 73-85, 2001
21 "Analysis for Buckling and Vibrations of Composite Stiffened Shells and Plates" 51 : 361-370, 2001
22 "A Quadrilateral Finite Element including Vertex Rotation for Plane Elasticity Analysis" 717-730, 1988
23 "A Differential Quadrature Analysis of Vibration for Rectangular Stiffened Plates" 241 (241): 247-252, 2001
24 "A Co-rotational 8-node Assumed Strain Shell Element for Postbuckling Analysis of Laminated Composite Plates and Shells" 30 (30): 330-342, 2003
25 "A 4-node Co-rotational ANS Shell Element forLaminated Composite Structures" 80 (80): 234-252, 2007