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| NO | Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date) |
|---|---|
| Dynamic model establishment of a deployable missile control fin with nonlinear hinge Kim, DK; Bae, JS; Lee, In; Han, Jae-Hung, JOURNAL OF SPACECRAFT AND ROCKETS, v.42, no.1, pp.66 - 77, 2005-01 | |
| Extension of flutter prediction parameter for multimode flutter systems Bae, JS; Kim, JY; Lee, In; Matsuzaki, Y; Inman, DJ, JOURNAL OF AIRCRAFT, v.42, no.1, pp.285 - 288, 2005-01 | |
| Linear and nonlinear aeroelastic analysis of fighter-type wing with control surface Bae, JS; Yang, SM; Lee, In, JOURNAL OF AIRCRAFT, v.39, no.4, pp.697 - 708, 2002 | |
| 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 | |
| Nonlinear aeroelastic analysis for a control fin with an actuator Shin, WH; Lee, In; Shin, YS; Bae, JS, JOURNAL OF AIRCRAFT, v.44, no.2, pp.597 - 605, 2007-03 | |
| 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 | |
| Flutter analysis of a wraparound fin projectile considering rolling motion Paek, SK; Bae, JS; Lee, In, JOURNAL OF SPACECRAFT AND ROCKETS, v.39, no.1, pp.66 - 72, 2002 |