Results 1-9 of 9 (Search time: 0.005 seconds).
NO | Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date) |
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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 | |
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 | |
Dynamic characteristics of ER fluid-filled composite plate using multielectrode configuration Cho, KD; Lee, In; Han, Jae-Hung, JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, v.16, no.5, pp.411 - 419, 2005-05 | |
Optical phase estimation for a patch-type extrinsic Fabry-Perot interferometer sensor system and its application to flutter suppression Kim, DH; Chang, YH; Han, Jae-Hung; Lee, In, SMART MATERIALS & STRUCTURES, v.14, no.4, pp.696 - 706, 2005-08 | |
Aeroelastic analysis of a wing with freeplay in the subsonic/transonic regions Yoo, JH; Park, YK; Lee, In; Han, Jae-Hung, JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING, v.48, no.2, pp.208 - 211, 2005-05 | |
Numerical investigation on the aeroelastic instability of a complete aircraft model Kim, JY; Kwon, HJ; Kim, KS; Lee, In; Han, Jae-Hung, JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING , v.48, no.2, pp.212 - 217, 2005-05 | |
Shape and vibration control of smart composite structures Lee, In; Roh, JH; Yang, SM; Han, Jae-Hung, ADVANCED COMPOSITE MATERIALS, v.14, no.2, pp.121 - 130, 2005 | |
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 | |
Vibration Measurement and Flutter Suppression Using Patch-type EFPI Sensor System Kim, Do-Hyung; Han, Jae-Hung; Lee, In, 한국항공우주학회지, v.6, no.1, pp.17 - 26, 2005-05 |
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