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| NO | Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date) |
|---|---|
| Effects of multiple structural nonlinearities on limit cycle oscillation of missile control fin Seo, Young-Jin; Lee, Seung-Jun; Bae, Jae-Sung; Lee, In, JOURNAL OF FLUIDS AND STRUCTURES, v.27, no.4, pp.623 - 635, 2011-05 | |
| Experimental studies on active shape control of composite structures using SMA actuators Yang, SM; Roh, JH; Han, Jae-Hung; Lee, In, JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, v.17, no.8-9, pp.767 - 777, 2006-08 | |
| Limit cycle oscillation of missile control fin with structural non-linearity Bae, JS; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.269, no.3-5, pp.669 - 687, 2004-01 | |
| Effects of actuator nonlinearity on aeroelastic characteristics of a control fin Shin, WH; Lee, SJ; Lee, In; Bae, JS, JOURNAL OF FLUIDS AND STRUCTURES, v.23, no.7, pp.1093 - 1105, 2007-10 | |
| Effects of structural nonlinearity on subsonic aeroelastic characteristics of an aircraft wing with control surface Bae, JS; Inman, DJ; Lee, In, JOURNAL OF FLUIDS AND STRUCTURES, v.19, no.6, pp.747 - 763, 2004-07 | |
| Aeroelastic analysis of composite rotor blades in hover Jeon, SM; Cho, MH; Lee, In, COMPUTERS STRUCTURES, v.66, no.1, pp.59 - 67, 1998-01 | |
| Aeroelastic analysis of bearingless rotors using large deflection beam theory Lim, IG; Lee, In, AIAA JOURNAL, v.45, no.3, pp.599 - 606, 2007-03 | |
| Characteristics of smart composite wing with SMA actuators and optical fiber sensors Yang, Seung-Man; Han, Jae-Hung; Lee, In, INTERNATIONAL JOURNAL OF APPLIED ELECTROMAGNETICS AND MECHANICS, v.23, no.3-4, pp.177 - 186, 2006 | |
| Configuration maintenance of inflated membrane structures using SMA film actuators Roh, Jin-Ho; Lee, In, CMES-COMPUTER MODELING IN ENGINEERING & SCIENCES, v.26, no.1, pp.13 - 30, 2008-03 |
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