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Results 11-20 of 31 (Search time: 0.003 seconds).

NO Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date)
11
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

12
Vibration Characteristics of Stiffened Laminated Plates Including Thermally Postbuckled Deflection

Lee, In; Lee, D.M, 3rd Asian-Pacific Conf. on Computational Mechanics, 1996

13
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

14
Vibration Charateristics and Control of Smart Composite Structures

Lee, In, Japan Society of Materials Science, 1998-06

15
Finite Element Analysis of Vibration and Damping for Symmetric Composite Laminates

Koo, K.N; Lee, In, Eighth International Conference on Composite Materials, 1991-07

16
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

17
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

18
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

19
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

20
Vibration Characteristics of Thermally Postbuckled Laminated Plates Using Finite Element Method

Lee, In; Lee, D.M, 25th FRP Symposium, 1996-03

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