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| NO | Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date) |
|---|---|
| Nonlinear flutter of aerothermally buckled composite shells with damping treatments Shin, Won-Ho; Oh, Il-Kwon; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.324, no.3-5, pp.556 - 569, 2009-07 | |
| DYNAMIC BEHAVIOR OF THICK COMPOSITE BEAMS KOO, KN; Lee, In, JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, v.14, no.3, pp.196 - 210, 1995-03 | |
| Vibration analysis of twisted cantilevered conical composite shells Lee, JJ; Yeom, CH; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.255, no.5, pp.965 - 982, 2002-08 | |
| An experimental study of active vibration control of composite structures with a piezo-ceramic actuator and a piezo-film sensor Han, Jae-Hung; Rew, KH; Lee, In, SMART MATERIALS & STRUCTURES, v.6, no.5, pp.549 - 558, 1997 | |
| SUPERSONIC FLUTTER ANALYSIS OF CLAMPED SYMMETRICAL COMPOSITE PANELS USING SHEAR DEFORMABLE FINITE-ELEMENTS Lee, In; CHO, MH, AIAA JOURNAL, v.29, no.5, pp.782 - 783, 1991-05 | |
| VIBRATION AND DAMPING ANALYSIS OF COMPOSITE LAMINATES USING SHEAR DEFORMABLE FINITE-ELEMENT KOO, KN; Lee, In, AIAA JOURNAL, v.31, no.4, pp.728 - 735, 1993-04 | |
| EFFECTS OF INPLANE DISPLACEMENTS ON FREQUENCY AND DAMPING OF COMPOSITE LAMINATES KOO, KN; Lee, In, AIAA JOURNAL, v.32, no.1, pp.221 - 223, 1994-01 | |
| Supersonic flutter analysis of stiffened isotropic and anisotropic panels Lee, DM; Lee, In, AIAA JOURNAL, v.34, no.3, pp.637 - 639, 1996-03 | |
| 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 | |
| FINITE-ELEMENT ANALYSIS OF COMPOSITE PANEL FLUTTER Lee, In; CHO, MH, COMPUTERS STRUCTURES, v.39, no.1-2, pp.165 - 172, 1991 |
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