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Results 1-10 of 18 (Search time: 0.003 seconds).

NO Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date)
1
Nonlinear Piezo-Hygro-Thermo-Elastic Behavior of Piezolaminated Composite Shells using Finite Element Method

Kundu, C. K; Han, Jae-Hung, 2008 KSAS-JSASS Joint Symposium on Aerospace Engineering, JSASS, KSAS, 2008-11-20

2
High-precision CTE Measurement System for the Structural Materials in Space Applications

Kim, H.-I; Han, Jae-Hung; Yang, H; Cho, C; Cho, H; Kim, H.-B, 2008 KSAS-JSASS Joint Symposium on Aerospace Engineering, JSASS, KSAS, 2008-11-20

3
Bio-inspired Design of Ornithopter

Han, Jae-Hung; Lee, J.-S; Kim, D.-K, US-KOREA Workshop and International Student Forum on Bio-Inspired Sensor Technology and Infra-Str., 2008-05-24

4
An aeroelastic analysis of a flexible flapping wing using modified strip theory

Kim, D.-K.; Lee, J.-S.; Lee, J.-Y.; Han, Jae-Hung, 15th SPIE International Symposium Smart Structures/NDE, v.6928, pp.69281O1 - 69281O8, 2008-03-10

5
Optical Fiber Sensor Technology for The Measurement of Structural Dynamic Shapes

Han, Jae-Hung; Kim, H.-I; Kang, L.-H, International Joint Conference of SMSAE/SMEBA 2008, SMSAE/SMEBA, 2008-07-23

6
Measurement of the Thermal Expansion for Space Structures Using Fiber Bragg Grating Sensors and Displacement Measuring

Kim, H.-I.; Kang, L.-H.; Han, Jae-Hung, ASME Conference on Smart Materials, Adaptive Structures and Intelligent Systems, SMASIS2008, pp.387 - 395, American Society of Mechanical Engineers, 2008-10-30

7
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

8
Dynamic Deformation Reconstruction of Aerospace Structures Using Fiber Bragg Granting Sensors

Han, Jae-Hung; Kang, Lae-Hyong, The International Symposium on Advanced Technology for High Performance Aircraft Core Parts Design, pp.63 - 66, International Symposium on Advanced Technology for High Performance Aircraft Core Parts Design, 2008-05

9
An Active Vibration Isolation System Using Piezoelectric Unimorph Actuators

Han, Jae-Hung; Kang, L.-H; Lee, J.-W, International Conference and Exhibition On New Actuators and Drive Systems, ACTUATOR, 2008-06-10

10
Filtering techniques in the dynamic deformation estimation using multiple strains measured by FBGs

Treiber, J.; Mueller, U.C.; Han, Jae-Hung; Baier, H., Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems 2008, pp.69322A1 - 69322A9, International Society for Optical Engineering (SPIE), 2008-03-10

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