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| NO | Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date) |
|---|---|
| VIBRATION ANALYSIS OF ANISOTROPIC PLATES WITH ECCENTRIC STIFFENERS LEE, DM; Lee, In, COMPUTERS STRUCTURES, v.57, no.1, pp.99 - 105, 1995-10 | |
| Supersonic flutter analysis of stiffened isotropic and anisotropic panels Lee, DM; Lee, In, AIAA JOURNAL, v.34, no.3, pp.637 - 639, 1996-03 | |
| A REFINED ANALYSIS OF VIBRATION AND DAMPING FOR ANISOTROPIC LAMINATES IN CYLINDRICAL BENDING KOO, KN; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.184, no.4, pp.553 - 566, 1995-07 | |
| STATIC AND DYNAMIC ANALYSIS OF COMPOSITE BOX BEAMS USING LARGE DEFLECTION THEORY JEON, SM; CHO, MH; Lee, In, COMPUTERS STRUCTURES, v.57, no.4, pp.635 - 642, 1995-11 | |
| VIBRATION ANALYSIS OF COMPOSITE WING WITH TIP MASS USING FINITE-ELEMENTS Lee, In; LEE, JJ, COMPUTERS STRUCTURES, v.47, no.3, pp.495 - 504, 1993-05 | |
| AEROELASTIC ANALYSIS OF A FLEXIBLE CONTROL SURFACE WITH STRUCTURAL NONLINEARITY Lee, In; Kim, SH, JOURNAL OF AIRCRAFT, v.32, no.4, pp.868 - 874, 1995-07 | |
| FINITE-ELEMENT ANALYSIS OF COMPOSITE PANEL FLUTTER Lee, In; CHO, MH, COMPUTERS STRUCTURES, v.39, no.1-2, pp.165 - 172, 1991 | |
| RESONANCE PREDICTION FOR CLOSED AND OPEN WIND-TUNNEL BY THE FINITE-ELEMENT METHOD Lee, In, AIAA JOURNAL, v.27, no.4, pp.391 - 398, 1989-04 | |
| A Patch-Type Smart Self-Sensing Actuator Chang, Young-Hwan; Kim, Do-Hyung; Lee, In; Han, Jae-Hung, Smart Materials and Structures, vol.15, no.3, pp.667-677, 2006-06 | |
| Study of a reduced and internally biased oxide wafer PZT actuator and its integration with shape memory alloy Shen, Xing; Han, Jae-Hung; Lee, In, SMART MATERIALS STRUCTURES, v.15, no.4, pp.89 - 93, 2006-08 |
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