Results 21-30 of 113 (Search time: 0.004 seconds).
NO | Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date) |
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Aeroelastic analysis of rotor systems using trailing edge flaps Lim, In-Gyu; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.321, no.3-5, pp.525 - 536, 2009-04 | |
Transonic Aeroelastic Analysis of All-Movable Wing with Free Play and Viscous Effects Kim, Jong-Yun; Kim, Kyung-Seok; Lee, In; Park, Young-Keun, JOURNAL OF AIRCRAFT, v.45, no.5, pp.1820 - 1824, 2008-09 | |
Aeroelastic analysis of a hingeless rotor blade in forward flight Jeon, Seong Min; Lee, In, AIAA Journal, Vol.38, No.5, pp.843-850, 2000-05 | |
Transonic and low-supersonic aerodynamic analysis of a wing with underpylon/store Kim, DH; Lee, In, JOURNAL OF AIRCRAFT, v.37, no.1, pp.189 - 192, 2000 | |
Numerical modeling of shape memory alloy thin film actuators and their applications Roh, Jin-Ho; Han, Jae-Hung; Lee, In, ADVANCED NONDESTRUCTUVE EVALUATION I, PTS 1 AND 2, PROCEEDINGS BOOK SERIES: KEY ENGINEERING MATERIALS, v.321-323, pp.186 - 191, 2006 | |
Nonlinear aeroelastic simulation of a full-span aircraft with oscillating control surfaces Yoo, JH; Kim, DH; Kwon, HJ; Lee, In, JOURNAL OF AEROSPACE ENGINEERING, v.18, no.3, pp.156 - 167, 2005-07 | |
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 | |
Dynamic Model Establishment of Deployable Missile Control Fin with Nonlinear Hinge Kim, Dae-Kwan; Lee, In; Han, Jae-Hung; Bae, Jae-Sung, Journal of Spacecraft and Rockets, vol.42, no.1, pp.66-77, 2005-01 | |
Online phase tracking of interferometric optical fiber sensors for vibration control Chang, YH; Kim, DH; Han, Jae-Hung; Lee, In, JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, v.18, no.4, pp.311 - 321, 2007-04 | |
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 |