Browse "AE-Journal Papers(저널논문)" by Subject PLATES
Showing results 21 to 38 of 38
| New Approach for Simple Prediction of Impact Force History on Composite Laminates i.h. choi; Hong, Chang Sun, AIAA JOURNAL, v.32, no.10, pp.2067 - 2072, 1994-01 |
| Nonlinear flutter of aerothermally buckled composite shells with damping treatments Shin, Won-Ho; Oh, Il-Kwon; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.324, no.3-5, pp.556 - 569, 2009-07 |
| Optimum design of composite structures with ply drop using genetic algorithm and expert system shell Kim, JS; Kim, Chun-Gon; Hong, Chang Sun, COMPOSITE STRUCTURES, v.46, no.2, pp.171 - 187, 1999-10 |
| Oscillatory behavior of supersonic impinging jet flows Kim, SI; Park, Seung O, SHOCK WAVES, v.14, no.4, pp.259 - 272, 2005-11 |
| Panel Flutter Emulation Using a Few Concentrated Forces Dhital, Kailash; Han, Jae-Hung, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.19, no.1, pp.80 - 88, 2018-03 |
| Practical design of tapered composite structures using the manufacturing cost concept Kim, JS; Kim, Chun-Gon; Hong, Chang Sun, COMPOSITE STRUCTURES, v.51, no.3, pp.285 - 299, 2001-03 |
| Progressive failure analysis for filament wound pressure vessel Doh, YD; Hong, Chang Sun, JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, v.14, no.12, pp.1278 - 1306, 1995-12 |
| SUPERSONIC FLUTTER ANALYSIS OF CLAMPED SYMMETRICAL COMPOSITE PANELS USING SHEAR DEFORMABLE FINITE-ELEMENTS Lee, In; CHO, MH, AIAA JOURNAL, v.29, no.5, pp.782 - 783, 1991-05 |
| Supersonic flutter analysis of stiffened isotropic and anisotropic panels Lee, DM; Lee, In, AIAA JOURNAL, v.34, no.3, pp.637 - 639, 1996-03 |
| The use of carbon/dielectric fiber woven fabrics as filters for electromagnetic radiation Lee, Sang-Eui; Park, Ki-Yeon; Oh, Kyoung-Sub; Kim, Chun-Gon, CARBON, v.47, no.8, pp.1896 - 1904, 2009-07 |
| 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 |
| 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 |
| 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 |
| VIBRATION ANALYSIS OF COMPOSITE WING WITH TIP MASS USING FINITE-ELEMENTS Lee, In; LEE, JJ, COMPUTERS STRUCTURES, v.47, no.3, pp.495 - 504, 1993-05 |
| 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 |
| VIBRATION AND DAMPING ANALYSIS OF COMPOSITE LAMINATES USING SHEAR DEFORMABLE FINITE-ELEMENT KOO, KN; Lee, In, AIAA JOURNAL, v.31, no.4, pp.728 - 735, 1993-04 |
| Vibration and Post-buckling Behavior of Laminated Composite Doubly Curved Shell Structures Kundu, Chinmay Kumar; Han, Jae-Hung, ADVANCED COMPOSITE MATERIALS, v.18, no.1, pp.21 - 42, 2009 |
| Vibration characteristics and snapping behavior of hygro-thermo-elastic composite doubly curved shells Kundu, CK; Han, Jae-Hung, COMPOSITE STRUCTURES, v.91, no.3, pp.306 - 317, 2009-12 |
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