Showing results 1 to 7 of 7
Aeroelastic Analysis of Helicopter Rotor System in Hover Yoo, SJ; Lim, IG; Lee, In; Kim, DH; Kim, DK, International Forum on Rotorcraft Multidisciplinary Technology for Dual-Use Applications, ROTOR KOREA, 2007-10-16 |
Aeroelastic Characteristics of Helicopter Rotor System in Hovering Flight Using Free-Wake Method Yoo, SJ; Lim, IG; Lee, In; Kim, DH; Kim, DK, 15th International Congress on Sound and Vibration, pp.2158 - 2165, KSNVE & IIAV, 2008-07-10 |
Dynamic model establishment of a deployable missile control fin with nonlinear hinge Kim, DK; Bae, JS; Lee, In; Han, Jae-Hung, JOURNAL OF SPACECRAFT AND ROCKETS, v.42, no.1, pp.66 - 77, 2005-01 |
Establishment of gun blast wave model and structural analysis for blast load Kim, DK; Han, Jae-Hung, JOURNAL OF AIRCRAFT, v.43, no.4, pp.1159 - 1168, 2006-07 |
Estimation of dynamic structural displacements using fiber Bragg grating strain sensors Kang, LH; Kim, DK; Han, Jae-Hung, JOURNAL OF SOUND AND VIBRATION, v.305, no.3, pp.534 - 542, 2007-08 |
Experimental investigation on the aerodynamic characteristics of a bio-mimetic flapping wing with macro-fiber composites Kim, DK; Kim, HI; Han, Jae-Hung; Kwon, KJ, JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, v.19, no.3, pp.423 - 431, 2008-03 |
Wind tunnel tests for a flapping wing model with a changeable camber using macro-fiber composite actuators Kim, DK; Han, Jae-Hung; Kwon, KJ, SMART MATERIALS & STRUCTURES, v.18, no.2, 2009-02 |
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