Dr TAY, Wee Beng, Senior Research Scientist, email: tsltaywb@nus.edu.sg Professional Affiliations Research Activities Research Interests Awards Selected Journal Publications Tay, W. B., & Lim, K. B. (2010). Numerical analysis of active chordwise flexibility on the performance of non-symmetrical flapping airfoils. Journal of Fluids and Structures, 26(1), 74–91. https://doi.org/10.1016/j.jfluidstructs.2009.10.005 Tay, W.-B., Tseng, Y.-H., Lin, L.-Y., & Tseng, W.-Y. (2011). Towards patient-specific cardiovascular modeling system using the immersed boundary technique. Biomedical Engineering Online, 10(1), 52. https://doi.org/10.1186/1475-925X-10-52. Tay, W. B., Bijl, H., & van Oudheusden, B. W. (2013). Biplane and tail effects in flapping flight. AIAA Journal, 51(9), 2133–2146. https://doi.org/10.2514/1.J052007. Tay, W. B., van Oudheusden, B. W., & Bijl, H. (2014). Numerical simulation of X-wing type biplane flapping wings in 3D using the immersed boundary method. Bioinspiration & Biomimetics, 9(3), 36001. https://doi.org/10.1088/1748-3182/9/3/036001. Tay, W. B., Deng, S., van Oudheusden, B. W., & Bijl, H. (2015). Validation of immersed boundary method for the numerical simulation of flapping wing flight. Computers & Fluids, 115, 226–242. https://doi.org/10.1016/j.compfluid.2015.04.009. Tay, W. B., van Oudheusden, B. W., & Bijl, H. (2015). Numerical simulation of a flapping four-wing micro-aerial vehicle. Journal of Fluids and Structures, 55, 237–261. https://doi.org/10.1016/j.jfluidstructs.2015.03.003. Tay, W. B. (2016). Symmetrical and non-symmetrical 3D wing deformation of flapping micro aerial vehicles. Aerospace Science and Technology, 55, 242–251. https://doi.org/10.1016/j.ast.2016.05.026. Tay, W. B. (2017). Effect of Different Types of Wing-Wing Interactions in Flapping MAVs. Journal of Bionic Engineering, 14, 60–74. Selected Conference Publications Tay, W. beng, de Baar, J. H. S., Percin, M., Deng, S., & van Oudheusden, B. W. (2016). Numerical simulation of a flapping wing MAV based on wing deformation capture analysis. In 34th AIAA Applied Aerodynamics Conference (pp. 1–13). Washington D.C. |