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Results 1-5 of 5 (Search time: 0.004 seconds).

NO Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date)
1
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

2
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

3
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

4
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

5
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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