Jae-Hung Han

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Junseong LeeSmall Launcher R&D Office, Korea Aerospace Research InstituteVerified email at kaist.ac.kr
Lae-Hyong KangJeonbuk National UniversityVerified email at jbnu.ac.kr
Jong-Seob HanChair of Aerodynamics and Fluid mechanics, Technical University of MunichVerified email at tum.de
Joong-Kwan KimDept. of Aerospace Eng., KAISTVerified email at kaist.ac.kr
Chun Gon KimKAISTVerified email at kaist.edu
Anh Tuan NguyenLe Quy Don Technical UniversityVerified email at lqdtu.edu.vn
ILKWON OHProfessor, Department of Mechanical Engineering, Korea Advanced Institute of Science andVerified email at kaist.ac.kr
Jong-Eun SuhPostdoctoral Researcher, California Institute of TechnologyVerified email at caltech.edu
Reynolds Addo-AkotoKorea Advanced Institute of Science and Technology (KAIST)Verified email at kaist.ac.kr
Jo Won ChangAeronautical Science and Flight Operation, Korea Aerospace UniversityVerified email at kau.ac.kr
Sang-Eui LeeInha UniversityVerified email at inha.ac.kr
Young Hwan ChangAssociate Professor, Dept. of Biomedical Engineering, Oregon Health and Science UniversityVerified email at ohsu.edu
Chinmay Kumar KunduAssociate ProfessorVerified email at kiit.ac.in
Jinhao QiuNanjing University of Aeronautics and AstronauticsVerified email at nuaa.edu.cn
Yoshiyuki KawamuraFukuoka Institute of TechnologyVerified email at fit.ac.jp
Andrew Jaeyong ChoiSenior Research Engineer at LG Electronics CTO | ICT Technology Center | Robot Cognition TPVerified email at lge.com
Jinbong KimKorea Institute of Materials ScienceVerified email at kims.re.kr
Prof Mahaveer KurkuriAssociate Director, Centre for Research in Functional Materials (CRFM), Jain UniversityVerified email at jainuniversity.ac.in
Norman M. WereleyUniversity of MarylandVerified email at umd.edu

Jae-Hung Han

Professor of Aerospace Engineering, KAIST

Verified email at kaist.edu - Homepage

Smart Materials Vibration Control Flapping-wing Air Vehicle


Title Sort by citations Sort by year Sort by title	Cited by Cited by	Year
Fabrication and electromagnetic characteristics of electromagnetic wave absorbing sandwich structures KY Park, SE Lee, CG Kim, JH Han Composites science and technology 66 (3-4), 576-584, 2006	366	2006
Optimal placement of piezoelectric sensors and actuators for vibration control of a composite plate using genetic algorithms JH Han, I Lee Smart Materials and Structures 8 (2), 257, 1999	290	1999
Estimation of dynamic structural displacements using fiber Bragg grating strain sensors LH Kang, DK Kim, JH Han Journal of sound and vibration 305 (3), 534-542, 2007	289	2007
Postbuckling and vibration characteristics of piezolaminated composite plate subject to thermo-piezoelectric loads IK Oh, JH Han, I Lee Journal of Sound and Vibration 233 (1), 19-40, 2000	161	2000
An experimental study of active vibration control of composite structures with a piezo-ceramic actuator and a piezo-film sensor JH Han, KH Rew, I Lee Smart Materials and Structures 6 (5), 549, 1997	154	1997
Displacement field estimation for a two-dimensional structure using fiber Bragg grating sensors S Rapp, LH Kang, JH Han, UC Mueller, H Baier Smart Materials and Structures 18 (2), 025006, 2009	141	2009
Fabrication and electromagnetic characteristics of microwave absorbers containing carbon nanofibers and NiFe particles KY Park, JH Han, SB Lee, JB Kim, JW Yi, SK Lee Composites Science and Technology 69 (7-8), 1271-1278, 2009	136	2009
Application of MWNT-added glass fabric/epoxy composites to electromagnetic wave shielding enclosures KY Park, SE Lee, CG Kim, JH Han Composite structures 81 (3), 401-406, 2007	135	2007
Analysis of composite plates with piezoelectric actuators for vibration control using layerwise displacement theory JH Han, I Lee Composites Part B: Engineering 29 (5), 621-632, 1998	126	1998
Microwave absorbing hybrid composites containing Ni–Fe coated carbon nanofibers prepared by electroless plating KY Park, JH Han, SB Lee, JW Yi Composites Part A: Applied Science and Manufacturing 42 (5), 573-578, 2011	104	2011
Shape estimation with distributed fiber Bragg grating sensors for rotating structures HI Kim, LH Kang, JH Han Smart Materials and Structures 20 (3), 035011, 2011	99	2011
Experimental investigation on the aerodynamic characteristics of a bio-mimetic flapping wing with macro-fiber composites DK Kim, HI Kim, JH Han, KJ Kwon Journal of intelligent material systems and structures 19 (3), 423-431, 2008	87	2008
Multi-modal vibration control using adaptive positive position feedback KH Rew, JH Han, I Lee Journal of intelligent material systems and structures 13 (1), 13-22, 2002	86	2002
Smart flapping wing using macrofiber composite actuators DK Kim, JH Han Smart Structures and Materials 2006: Smart Structures and Integrated Systems …, 2006	83	2006
Thermal post-buckling analysis of shape memory alloy hybrid composite shell panels JH Roh, IK Oh, SM Yang, JH Han, I Lee Smart Materials and Structures 13 (6), 1337, 2004	79	2004
Ornithopter flight simulation based on flexible multi-body dynamics AT Pfeiffer, JS Lee, JH Han, H Baier Journal of Bionic Engineering 7 (1), 102-111, 2010	73	2010
An aeroelastic analysis of a flexible flapping wing using modified strip theory DK Kim, JS Lee, JY Lee, JH Han Active and Passive Smart Structures and Integrated Systems 2008 6928, 69281O, 2008	73	2008
Aeroelastic characteristics of cylindrical hybrid composite panels with viscoelastic damping treatments WH Shin, IK Oh, JH Han, I Lee Journal of Sound and Vibration 296 (1-2), 99-116, 2006	73	2006
Wind tunnel tests for a flapping wing model with a changeable camber using macro-fiber composite actuators DK Kim, JH Han, KJ Kwon Smart materials and structures 18 (2), 024008, 2009	69	2009
Active flutter suppression of a lifting surface using piezoelectric actuation and modern control theory JH Han, J Tani, J Qiu Journal of Sound and Vibration 291 (3-5), 706-722, 2006	68	2006

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