Nonlinear aeroelasticity of a very flexible blended-wing-body aircraft W Su, CES Cesnik Journal of Aircraft 47 (5), 1539-1553, 2010 | 220 | 2010 |
Nonlinear aero-elasticity of a very flexible blended-wing-body aircraft W Su, CES Cesnik 50th A1AA/ASCE/AHS/ASC Structure, Structural Dynamics, and Materials …, 2009 | 220 | 2009 |
Dynamic response of highly flexible flying wings W Su, CES Cesnik Proceedings of the 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural …, 2006 | 210* | 2006 |
Dynamic response of highly flexible flying wings W Su, CES Cesnik AIAA Journal 49 (2), 324-339, 2011 | 174 | 2011 |
Strain-based geometrically nonlinear beam formulation for modeling very flexible aircraft W Su, CES Cesnik International Journal of Solids and Structures 48 (16-17), 2349-2360, 2011 | 133 | 2011 |
Nonlinear aeroelastic modeling and analysis of fully flexible aircraft CES Cesnik, W Su Paper No. AIAA-2005-2169, Proceedings of the 46th AIAA/ASME/ASCE/AHS/ASC …, 2005 | 109 | 2005 |
X-HALE: A Very Flexible Unmanned Aerial Vehicle for Nonlinear Aeroelastic Tests CES Cesnik, PJ Senatore, W Su, EM Atkins, CM Shearer AIAA Journal 50 (12), 2820-2833, 2012 | 106 | 2012 |
Flutter suppression for highly flexible wings using passive and active piezoelectric effects N Tsushima, W Su Aerospace Science and Technology 65, 78-89, 2017 | 91 | 2017 |
Geometrically nonlinear static aeroelastic analysis of composite morphing wing with corrugated structures N Tsushima, T Yokozeki, W Su, H Arizono Aerospace Science and Technology 88, 244-257, 2019 | 76 | 2019 |
Coupled nonlinear aeroelasticity and flight dynamics of fully flexible aircraft W Su University of Michigan, 2008 | 73 | 2008 |
Nonlinear aeroelastic simulation of X-HALE: a very flexible UAV CES Cesnik, W Su 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2011 | 48 | 2011 |
X-HALE: A very flexible UAV for nonlinear aeroelastic tests C Cesnik, P Senatore, W Su, E Atkins, C Shearer, N Pitchter 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2010 | 45 | 2010 |
A study on adaptive vibration control and energy conversion of highly flexible multifunctional wings N Tsushima, W Su Aerospace Science and Technology 79, 297-309, 2018 | 44 | 2018 |
Strain-Based Analysis for Geometrically Nonlinear Beams: A Modal Approach W Su, CES Cesnik Journal of Aircraft 51 (3), 890-903, 2014 | 44 | 2014 |
Smooth-switching LPV control for vibration suppression of a flexible airplane wing T He, GG Zhu, SSM Swei, W Su Aerospace Science and Technology 84, 895-903, 2019 | 43 | 2019 |
Modeling of highly flexible multifunctional wings for energy harvesting N Tsushima, W Su Journal of Aircraft 53 (4), 1033-1044, 2016 | 41 | 2016 |
Flight dynamic stability of a flapping wing micro air vehicle in hover W Su, CES Cesnik AIAA Structures, Structural Dynamics, and Materials Conference, 2011-2009, 2011 | 40 | 2011 |
Application of ICC LPV control to a blended-wing-body airplane with guaranteed H∞ performance T He, AK Al-Jiboory, GG Zhu, SSM Swei, W Su Aerospace Science and Technology 81, 88-98, 2018 | 35 | 2018 |
LPV modeling of a flexible wing aircraft using modal alignment and adaptive gridding methods AK Al-Jiboory, G Zhu, SSM Swei, W Su, NT Nguyen Aerospace Science and Technology 66, 92-102, 2017 | 35 | 2017 |
Concurrent active piezoelectric control and energy harvesting of highly flexible multifunctional wings N Tsushima, W Su Journal of Aircraft 54 (2), 724-736, 2017 | 33 | 2017 |