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Numerical Simulations of Two-Dimensional Vortex-Body Interaction Using a Vortex Method Lee, Duck-Joo; Park, J. H., The 3rd JSME-KSME Fluids Engineering Conference, 1994-07 |
두꺼운 복합적층보의 동적특성에 대한 실험 및 유한요소 해석 구교남; 이인, 한국항공우주학회 추계학술발표회 , 한국항공우주학회, 1993-11 |
Aeroelastic Characteristics of a Control Surface with Structural Nonlinearity Lee, In; Kim, S. H, The First International Conference on Flow Interaction, 1994-09 |
Experiment and Numerical Analysis of Dynamic Characteristics of Thick Composite Beams Lee, In; Koo, K. N, Advancing with Composites, 1994-05 |
Flutter Analysis for Control Surface of Launch Vehicle with Dynamic Stiffness Lee, In; Paek, S. K, International Conference on Aero-Hydroelasticity, 1993-10 |
Static Aeroelastic Behavior of Various Planform Wings Kim, S. H.; Lee, In, Proceedings of the 26th Aircraft Symposium of the Japan Society for Aeronautical and Space Sciences, the Japan Society for Aeronautical and Space Sciences, 1988-10 |
복합재료 평판 날개의 정적 공탄성 특성에 관한 실험적 연구 양성모; 이인, 한국항공우주학회 추계학술발표회, 한국항공우주학회, 1992-11 |
Application of Panel Method Aerodynamics to Rotor Aeroelasticity in Hover Kwon, Oh Joon; Hodges, D. H., AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference, 1989-04 |
Spring-in of Composite Laminated Bends Kim, Chun-Gon; Kim, TW; Kim, IG; Jun, EJ, Proceedings of ICCM-VII, v.1, pp.83 - 88, International Conference on Composite Materials(ICCM), 1989 |
Active vibration control of a deploying appendage using piezoelectric sensors and actuators Bang, Hyochoong; Agrawal, BN, AAS/AIAA Astrodynamics Specialist Conference, 1993-08 |
Postbuckling compressive strength of graphite/epoxy laminated cylindrical panels loaded in compression Kweon J.H.; Hong, Chang Sun; Lee I.C., The 35th AIAA Structures, Structural Dynamics, and Materials Conference, v.1, pp.290 - 298, 1994-04-18 |
복합재료 항공기 날개의 공탄성 현상 이인, 한국항공우주학회 춘계학술발표회, 한국항공우주학회, 1993-04 |
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Dynamics of an Unsteady Ethylene Jet Diffusion Flame Kaplan, CR; Baek, Seung-Wook; Ellezey, JL; Oran, ES, ESS Meeting of the Combustion Institute, 1991-10 |
Vibration Analysis of Composite Plate Wing Lee, J. J; Lee, In, Proceedings of the 27th Aircraft Symposium of the Japan Society for Aeronautical and Space Sciences, the Japan Society for Aeronautical and Space Sciences, 1989-10 |
Application of a Panel Method to Aeroelastic Stability of Rotors in Hover Kwon, Oh Joon; Hodges, D. H; Peters, D. A; Sankar, L. N, International Symposium on Boundary Element Method : Advances in Solid and Fluid Mechanics, 1989-10 |
비대칭날개를 갖는 비행체의 형상에 따른 공력계수변화 유기완; 이덕주; 안창수, 항공우주학회 93년 춘계학술발표회, pp.183 - 186, 한국항공우주학회, 1993-04-01 |
Postbuckling behaviour of graphite/epoxy laminated cylindrical panels under axial compression Hong, Chang Sun; Kweon J.H., Proceedings of the International Conference on Advanced Composite Materials, pp.247 - 252, 1993-02-15 |
Active vibration control of flexible space structures by using piezoelectric sensors and actuators Agrawal, BN; Bang, Hyochoong, 14th Biennial ASME Conference, pp.169 - 179, 1993-09-19 |
비행기 기본 설계용 CAE 시스템 개발 연구 임승영; 김종암; 명노신; 선병찬; 임철호; 류동영; 구훤준; et al, '91 한국항공우주학회 추계학술발표회, 한국항공우주학회, 1991-11 |
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