Author:
Masud Mahadi Hasan,Dabnichki Peter
Publisher
Springer Nature Switzerland
Reference17 articles.
1. Airfoil Tools. (2022). NACA 4 digit Airfoil database. Available at http://airfoiltools.com/search/index?m%5Bgrp%5D=naca4d&m%5Bsort%5D=1. Accessed 4 Apr 2022.
2. Akbari, M. H., & Price, S. J. (2003). Simulation of dynamic stall for a NACA 0012 airfoil using a vortex method. Journal of Fluids and Structures. Elsevier, 17(6), 855–874.
3. Bearman, P. W., & Owen, J. C. (1998). Reduction of bluff-body drag and suppression of vortex shedding by the introduction of wavy separation lines. Journal of Fluids and Structures. Elsevier, 12(1), 123–130.
4. Cai, C., Liu, S., Zuo, Z., Maeda, T., Kamada, Y., Li, Q. A., & Sato, R. (2019). Experimental and theoretical investigations on the effect of a single leading-edge protuberance on airfoil performance. Physics of Fluids. AIP Publishing LLC, 31(2), 27103.
5. Critzos, C. C., Heyson, H. H., & Boswinkle, R. W., Jr. (1955). Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 deg to 180 deg. National Aeronautics and Space Administration.