Lasauskas, Eduardas, Thorsten Lutz, and Markus Dietz. “Influence of Trailing Edge Tab on Moment Characteristics of NACA 23012 Airfoil”. Aviation 11, no. 4 (December 31, 2007): 3-8. Accessed April 27, 2024. https://journals.vilniustech.lt/index.php/Aviation/article/view/7051.