Browse "Dept. of Aerospace Engineering(항공우주공학과)" by Author Oh, Il-Kwon

Showing results 15 to 29 of 29

15
Postbuckling and vibration characteristics of piezolaminated composite plate subject to thermo-piezoelectric loads

Oh, Il-Kwon; Han, Jae-Hung; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.233, no.1, pp.19 - 40, 2000-05

16
Stabilization of thermoelastic unstable postbuckling in cylindrical piezolaminated panels

Oh, Il-Kwon; Whang, Won-Gul; Kim, Dong-Hyun; Lee, In, Key Engineering Materials, v.334-335, no.2, pp.1009 - 1012, Trans Tech Publications Ltd., 2007-03

17
Supersonic flutter analysis of stiffened laminated plates subject to thermal load

Lee, In; Lee, DM; Oh, Il-Kwon, JOURNAL OF SOUND AND VIBRATION, v.224, no.1, pp.49 - 67, 1999-07

18
Supersonic flutter suppression of piezolaminated cylindrical panels based on multifield layerwise theory

Oh, Il-Kwon; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.291, no.3-5, pp.1186 - 1201, 2006-04

19
Thermal post-buckled behaviors of cylindrical composite shells with viscoelastic damping treatments

Shin, Won-Ho; Lee, Seung-Jun; Oh, Il-Kwon; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.323, no.1-2, pp.93 - 111, 2009-06

20
Thermal post-buckling analysis of shape memory alloy hybrid composite shell panels

Roh, JH; Oh, Il-Kwon; Yang, SM; Han, Jae-Hung; Lee, In, SMART MATERIALS & STRUCTURES, v.13, no.6, pp.1337 - 1344, 2004-12

21
Thermal post-buckling behavior of patched laminated panels under uniform and non-uniform temperature distributions

Lee, JJ; Oh, Il-Kwon; Lee, In; Yeom, CH, COMPOSITE STRUCTURES, v.55, no.2, pp.137 - 145, 2002-02

22
Thermal snapping and vibration characteristics of cylindrical composite panels using layerwise theory

Oh, Il-Kwon; Lee, In, COMPOSITE STRUCTURES, v.51, no.1, pp.49 - 61, 2001-01

23
Thermoelastic and aeroelastic stability analyses of piezolaminated composite structures based on layerwise nonlinear finite elements = 층별변위 비선형 유한요소법에 기초한 압전복합적층 구조물의 열탄성 및 공력탄성 안정성 해석link

Oh, Il-Kwon; 오일권; et al, 한국과학기술원, 2001

24
Thermopiezoelastic Postbuckling and Vibration Analysis of Piezolaminated Plate Using Layerwise Theory

Oh, Il-Kwon; Han, Jae-Hung; Lee, In, The Second Asian-Australasian Conference on Composite Materials, ACCM, 2000-08

25
Thermopiezoelastic snapping of piezolaminated plates using layerwise nonlinear finite elements

Oh, Il-Kwon; Han, Jae-Hung; Lee, In, AIAA JOURNAL, v.39, no.6, pp.1188 - 1197, 2001-06

26
Ultrasonic Active Fiber Sensor based on Pulse-echo Method

Lim, Seung-Hyun; Oh, Il-Kwon; Lee, Jung-Ryul, JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, v.20, no.9, pp.1035 - 1043, 2009-06

27
Vibration and Damping Analysis of Cylindrical Hybrid Composite Panels with Viscoelastic Layer

Oh, Il-Kwon; Kim, D.H; Shin, W.H; Lee, In; Koo, K.N, 3rd ACCM(Asian-Australasian Conference on Composite Materials)2002, ACCM, 2002-07

28
Vibration and Flutter Characteristics of Stiffened Composite Plate Considering Thermal Effect

Lee, In; Oh, Il-Kwon; Lee, D.M, 1997 International Mechanical Engineering Congress & Exposition, 1997-11

29
비선형 거동을 고려한 복합적층 패널의 공력열탄성 해석 = Aerothermoelastic analysis of composite laminated panel considering nonlinear behaviorlink

오일권; Oh, Il-Kwon; et al, 한국과학기술원, 1997

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