| A paper-based device for performing loop-mediated isothermal amplification with real-time simultaneous detection of multiple DNA targets Y Seok, HA Joung, JY Byun, HS Jeon, SJ Shin, S Kim, YB Shin, HS Han, ... Theranostics 7 (8), 2220, 2017 | 158 | 2017 |
| Effect of manufacturing methods on the shear strength of composite single-lap bonded joints MG Song, JH Kweon, JH Choi, JH Byun, MH Song, SJ Shin, TJ Lee Composite Structures 92 (9), 2194-2202, 2010 | 133 | 2010 |
| On the modeling of integrally actuated helicopter blades CES Cesnik, S Shin International Journal of Solids and Structures 38 (10-13), 1765-1789, 2001 | 131 | 2001 |
| Vibratory loads reduction testing of the NASA/Army/MIT active twist rotor ML Wilbur, PH Mirick, WT Yeager, CW Langston, CES Cesnik, SJ Shin Journal of the American Helicopter Society 47 (2), 123-133, 2002 | 130 | 2002 |
| Dynamic response of active twist rotor blades CES Cesnik, SJ Shin, ML Wilbur Smart materials and structures 10 (1), 62, 2001 | 96 | 2001 |
| Integral twist actuation of helicolpter rotor blades for vibration reduction SJ Shin Massachusetts Institute of Technology, 2001 | 59 | 2001 |
| On the twist performance of a multiple-cell active helicopter blade CES Cesnik, SJ Shin Smart Materials and Structures 10 (1), 53, 2001 | 58 | 2001 |
| Closed‐Loop Control Test of the NASA/Army/MIT Active Twist Rotor for Vibration Reduction SJ Shin, CES Cesnik, SR Hall Journal of the American Helicopter Society 50 (2), 178-194, 2005 | 52 | 2005 |
| Modeling, Design, and Testing of the NASA/ARMY/MIT Active Twist Rotor Prototype Blade CES Cesnik, S Shin, WK Wilkie, ML Wilbur, PH Mirick AHS International Annual Forum, 55 th, Montreal, Canada, 533-544, 1999 | 43 | 1999 |
| Effects of camber angle on aerodynamic performance of flapping-wing micro air vehicle SH Yoon, H Cho, J Lee, C Kim, SJ Shin Journal of Fluids and Structures 97, 103101, 2020 | 40 | 2020 |
| Aeroelastic analysis of the NASA/Army WK Wilkie, ML Wilbur, PH Mirick, CES Cesnik, SJ Shin MIT active twist rotor. In American Helicopter Society 55th Forum, Montreal …, 1999 | 38 | 1999 |
| Structural dynamic modeling for rotating blades using three dimensional finite elements YJ Kee, SJ Shin Journal of Mechanical Science and Technology 29, 1607-1618, 2015 | 37 | 2015 |
| Geometrically nonlinear dynamic formulation for three-dimensional co-rotational solid elements H Cho, H Kim, SJ Shin Computer Methods in Applied Mechanics and Engineering 328, 301-320, 2018 | 35 | 2018 |
| Wind turbine blade optimal design considering multi-parameters and response surface method SL Lee, SJ Shin Energies 13 (7), 1639, 2020 | 34 | 2020 |
| Design and analysis of the link mechanism for the flapping wing MAV using flexible multi-body dynamic analysis JH Jeon, H Cho, Y Kim, JH Lee, DH Gong, SJ Shin, C Kim International Journal of Micro Air Vehicles 9 (4), 253-269, 2017 | 34 | 2017 |
| Optimum design framework for integrally twisted helicopter blades C Cesnik, J Mok, A Parikh, SJ Shin 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials …, 2004 | 33 | 2004 |
| Vibratory loads reduction testing of the NASA/ARMY/MIT Active Twist Rotor ML Wilbur, PH Mirick, WT Yeager Jr, CW Langston, CES Cesnik, SJ Shin | 33 | 2001 |
| Design and manufacturing of a model-scale active twist rotor prototype blade SJ Shin, CES Cesnik, WK Wilkie, ML Wilbur Journal of Intelligent Material Systems and Structures 19 (12), 1443-1456, 2008 | 32 | 2008 |
| Hover testing of the NASA/ARMY/MIT active twist rotor prototype blade ML Wilbur, WT Yeager Jr, WK Wilkie, CES Cesnik, SJ Shin | 32 | 2000 |
| Effect of flexibility on flapping wing characteristics in hover and forward flight N Lee, S Lee, H Cho, SJ Shin Computers & Fluids 173, 111-117, 2018 | 31 | 2018 |
