Weihua Su, Ph.D.
Affiliations: | 2008 | University of Michigan, Ann Arbor, Ann Arbor, MI |
Area:
Aerospace EngineeringGoogle:
"Weihua Su"Parents
Sign in to add mentorCarlos E. S. Cesnik | grad student | 2008 | University of Michigan | |
(Coupled nonlinear aeroelasticity and flight dynamics of fully flexible aircraft.) |
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Publications
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Hang X, Su W, Fei Q, et al. (2020) Analytical sensitivity analysis of flexible aircraft with the unsteady vortex-lattice aerodynamic theory Aerospace Science and Technology. 99: 105612 |
Su W, Song W. (2019) A real-time hybrid aeroelastic simulation platform for flexible wings Aerospace Science and Technology. 95: 105513 |
Tsushima N, Yokozeki T, Su W, et al. (2019) Geometrically nonlinear static aeroelastic analysis of composite morphing wing with corrugated structures Aerospace Science and Technology. 88: 244-257 |
He T, Zhu GG, Swei SS-, et al. (2019) Smooth-switching LPV control for vibration suppression of a flexible airplane wing Aerospace Science and Technology. 84: 895-903 |
He T, Al-Jiboory AK, Zhu GG, et al. (2018) Application of ICC LPV control to a blended-wing-body airplane with guaranteed H∞ performance Aerospace Science and Technology. 81: 88-98 |
Tsushima N, Su W. (2018) A study on adaptive vibration control and energy conversion of highly flexible multifunctional wings Aerospace Science and Technology. 79: 297-309 |
Hammerton JR, Su W, Zhu G, et al. (2018) Optimum distributed wing shaping and control loads for highly flexible aircraft Aerospace Science and Technology. 79: 255-265 |
Al-Jiboory AK, Zhu G, Swei SS, et al. (2017) LPV Modeling of a Flexible Wing Aircraft Using Modal Alignment and Adaptive Gridding Methods. Aerospace Science and Technology. 66: 92-102 |
Su W. (2017) Development of an Aeroelastic Formulation for Deformable Airfoils Using Orthogonal Polynomials Aiaa Journal. 55: 2793-2807 |
Tsushima N, Su W. (2017) Concurrent Active Piezoelectric Control and Energy Harvesting of Highly Flexible Multifunctional Wings Journal of Aircraft. 54: 724-736 |