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NO	Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date)
1	THE WING-BODY AEROELASTIC ANALYSES USING THE INVERSE DESIGN METHOD Lee, Seung-Jun; Im, Dong-Kyun; Lee, In; Kwon, Jang-Hyuk, MODERN PHYSICS LETTERS B, v.24, no.13, pp.1479 - 1482, 2010-05
2	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
3	Aeroelastic response and stability analysis of composite rotor blades in forward flight Jeon, SM; Lee, In, COMPOSITES PART B-ENGINEERING, v.32, no.3, pp.249 - 257, 2001
4	Frequency and time domain flutter computations of a wing with oscillating control surface including shock interference effects Kwon, HJ; Kim, DH; Lee, In, AEROSPACE SCIENCE AND TECHNOLOGY, v.8, no.6, pp.519 - 532, 2004-09
5	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

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