Results 11-20 of 31 (Search time: 0.003 seconds).
NO | Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date) |
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Aeroelastic Stability of a Hingeless Rotor Blade in Hover Using Finite Elements Based on Large Deflection Theory Lee, In; Cho, M. H, Holt Ashley Symposium, 1993-09 | |
Vibration Characteristics of Stiffened Laminated Plates Including Thermally Postbuckled Deflection Lee, In; Lee, D.M, 3rd Asian-Pacific Conf. on Computational Mechanics, 1996 | |
Optimal Placement of Piezoelectric Acutuators and Control of Intelligent Structures Lee, In, International Workshop on Intelligent Fluid and Material System, Institute of Fluid Science, 1996-08 | |
Vibration Charateristics and Control of Smart Composite Structures Lee, In, Japan Society of Materials Science, 1998-06 | |
Finite Element Analysis of Vibration and Damping for Symmetric Composite Laminates Koo, K.N; Lee, In, Eighth International Conference on Composite Materials, 1991-07 | |
Aeroelastic Response and Stability Analysis of Composite Rotor Blade in Forward Flight Jeon, S.M; Lee, In, 1999 ASME Mechanics and Materials Conference, ASME, 1999-06 | |
Vibration and Flutter Characteristics of Stiffened Composite Plate Considering Thermal Effect Lee, In; Oh, Il-Kwon; Lee, D.M, 1997 International Mechanical Engineering Congress & Exposition, 1997-11 | |
Flutter analysis of composite panels in supersonic flow Lee, In; Cho, Maeng-Hyo, 31st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Part 3 (of 4): Structural Dynamics I, pp.1540 - 1550, 1990-04-02 | |
Static Aeroelastic Analysis of Composite Wing Lee, In; Kim, S. H; Hong, Chang Sun; Miura, H., Proc. of the 17th Congress of International Council of the Aeronautical Sciences(ICAS), pp.594 - 601, 1990-09 | |
Vibration Characteristics of Thermally Postbuckled Laminated Plates Using Finite Element Method Lee, In; Lee, D.M, 25th FRP Symposium, 1996-03 |