Biologically Inspired Wing Leading Edge for Enhanced Wind Turbine and Aircraft Performance
Computational fluid dynamics simulations of tubercled leading edge wings are analyzed to determine the underlying mechanisms that may lead to potential performance improvements of wind turbines and aircraft. Reasons for performance improvements suggested in previous studies can probably be attributed to the formation of a complex vortex structure on the tubercled wings. A local trailing vortex cancelation mechanism is proposed to explain performance improvements of finite wings
T. A. Swanson and K. M. Isaac, "Biologically Inspired Wing Leading Edge for Enhanced Wind Turbine and Aircraft Performance," Proceedings of the 6th AIAA Theoretical Fluid Mechanics Conference Proceedings (2011, Honolulu, HI), American Institute of Aeronautics and Astronautics (AIAA), Jun 2011.
The definitive version is available at https://doi.org/10.2514/6.2011-3533
6th AIAA Theoretical Fluid Mechanics Conference, AIAA ARC (2011: Jun. 27-30, Honolulu, HI)
Mechanical and Aerospace Engineering
Article - Conference proceedings
© 2011 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
30 Jun 2011