Browse "Dept. of Aerospace Engineering(항공우주공학과)" by Author Kim, Dae-Kwan
Showing results 1 to 17 of 17
| Dynamic Model Establishment of a Deployable Missile Control Fin with Nonlinear Hinge Kim, Dae-Kwan; Bae, Jae-Sung; Lee, In; Han, Jae-Hung, Journal of Spacecraft and Rockets, vol.42, no.1, pp.66-77, 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 |
| Establishment of Gun Blast Wave Model and Structural Analysis for Blast Load Kim, Dae-Kwan; Han, Jae-Hung, 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, 2005-04 |
| Experimental Investigation on the Aerodynamic Characteristics of a Bio-mimetic Flapping Wing with Macro-Fiber Composites Kim, Dae-Kwan; Kim, Hong-Il; Han, Jae-Hung; Kwon, Ki-Jung, Smart Materials for Engineering & Biomedical Application, 2006-09 |
| Ground Tracking Support Condition Effect on Orbit Determination for Korea Pathfinder Lunar Orbiter (KPLO) in Lunar Orbit Kim, Young-Rok; Song, Young-Joo; Park, Jae-ik; Lee, Donghun; Bae, Jonghee; Hong, SeungBum; Kim, Dae-Kwan; et al, JOURNAL OF ASTRONOMY AND SPACE SCIENCES, v.37, no.4, pp.237 - 247, 2020-12 |
| Improved Aerodynamic Model for Efficient Analysis of Flapping-Wing Flight Kim, Dae-Kwan; Lee, Jun-Seong; Han, Jae-Hung, AIAA JOURNAL, v.49, no.4, pp.868 - 872, 2011-04 |
| Longitudinal Flight Dynamics of Bioinspired Ornithopter Considering Fluid-Structure Interaction Lee, Jun-Seong; Kim, Joong-Kwan; Kim, Dae-Kwan; Han, Jae-Hung, JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.34, no.3, pp.667 - 677, 2011 |
| Nonlinear aeroelastic analysis of a deployable missile control fin Bae, Jae-Sung; Kim, Dae-Kwan; Shin, Won-Ho; Lee, In; Kim, Seung-Ho, JOURNAL OF SPACECRAFT AND ROCKETS, v.41, no.2, pp.264 - 271, 2004-03 |
| Optimal Design of a Flexible Flapping Wing Using Fluid-Structure Interaction Analysis Han, Jae-Hung; Kim, Dae-Kwan, The 8th International Conference on Motion and Vibration Control (MOVIC), MOtion and VIbration Control(MOVIC), 2008-09 |
| Overview of the Flight Dynamics Subsystem for Korea Pathfinder Lunar Orbiter Mission Song, Young-Joo; Kim, Young-Rok; Bae, Jonghee; Park, Jae-ik; Hong, Seungbum; Lee, Donghun; Kim, Dae-Kwan, AEROSPACE, v.8, no.8, 2021-08 |
| Practical Algorithms on Lunar Reference Frame Transformations for Korea Pathfinder Lunar Orbiter Flight Operation Song, Young-Joo; Lee, Donghun; Kim, Young-Rok; Bae, Jonghee; Park, Jae-ik; Hong, SeungBum; Kim, Dae-Kwan; et al, JOURNAL OF ASTRONOMY AND SPACE SCIENCES, v.38, no.3, pp.185 - 192, 2021-09 |
| Study of flapping actuator modules using IPMC Kim, Hong-Il; Kim, Dae-Kwan; Han, Jae-Hung, Proc. SPIE, Vol. 6524, 65241A, 2007-03 |
| Substructure synthesis method for a nonlinear structure with a sliding mode condition Kim, Dae-Kwan; Lee, Min-Su; Han, Jae-Hung, JOURNAL OF SOUND AND VIBRATION, v.321, no.3-5, pp.704 - 720, 2009-04 |
| Wind Tunnel Tests for a Flapping Wing Model with Changeable Camber Using Macro-Fber Composite Actuators (Invited Paper) Han, Jae-Hung; Kim, Dae-Kwan; Kwon, Ki-Jung, International Conference on Smart Materials and Nanotechnology in Engineering, The International Society for Optical Engineering, 2007-07 |
| 날갯짓 비행체의 공력특성에 관한 실험적 연구 김, 대관; 김, 홍일; 한, 재흥; Kim, Dae-Kwan; Kim, Hong-Il; Han, Jae-Hung, 한국항공우주학회 춘계학술발표회 논문집, 2006-04 |
| 비선형 힌지를 갖는 접는 미사일 조종날개에 대한 모델 수립 및 동적 특성 = Dynamic characteristics and model establishment of deployable missile control fin with nonlinear hingelink 김대관; Kim, Dae-Kwan; et al, 한국과학기술원, 2003 |
| 유연한 플래핑 날개의 공탄성 특성 및 유체-구조 연계해석에 관한 연구 = A study on aeroelastic characteristics and fluid-structure interaction of a flexible flapping winglink 김대관; Kim, Dae-Kwan; et al, 한국과학기술원, 2008 |
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