Showing results 1 to 10 of 10
Development of an UAV with a variable-span morphing wing Bae, Jae-Sung; Kim, Jong-Hwan; Lee, Soo-Yong; Park, Jung-Sun; Kim, Jin-Sung; Lee, In, 16th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015, International Forum on Aeroelasticity and Structural Dynamics (IFASD), 2015-08 |
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 |
Effect of Inboard and Outboard Folding Angles on Aeroelastic Characteristics of a Folding Wing Shrestha, Pratik; Jeong, Min-Soo; Kim, Eun-Ho; Lee, In; Bae, Jae-Sung, 한국항공우주학회 추계학술대회, 한국항공우주학회, 2012-11-15 |
Effects of multiple structural nonlinearities on limit cycle oscillation of missile control fin Seo, Young-Jin; Lee, Seung-Jun; Bae, Jae-Sung; Lee, In, JOURNAL OF FLUIDS AND STRUCTURES, v.27, no.4, pp.623 - 635, 2011-05 |
Effects of shape memory alloys on low velocity impact characteristics of composite plate Kim, Eun-Ho; Lee, In; Roh, Jin-Ho; Bae, Jae-Sung; Choi, Ik-Hyeon; Koo, Kyo-Nam, COMPOSITE STRUCTURES, v.93, no.11, pp.2903 - 2909, 2011-10 |
LOW-VELOCITY IMPACT CHARACTERISTICS OF COMPOSITE PLATES WITH SHAPE MEMORY ALLOY WIRES Rim, Mi-Sun; Kim, Eun-Ho; Lee, In; Choi, Ik-Hyeon; Ahn, Seok-Min; Koo, Kyo-Nam; Bae, Jae-Sung; et al, JOURNAL OF THEORETICAL AND APPLIED MECHANICS, v.49, no.3, pp.841 - 857, 2011-04 |
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 |
구조 비선형성을 고려한 공탄성 특성 및 플러터 억제 = Aeroelastic characteristics and flutter suppression considering structural nonlinearitylink 배재성; Bae, Jae-Sung; et al, 한국과학기술원, 2002 |
오일러 방정식을 이용한 2차원 캐스케이드 플러터 해석 = Flutter analysis of two-dimensional cascade using euler equationslink 배재성; Bae, Jae-Sung; et al, 한국과학기술원, 1998 |
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