BHATNAGAR, K.; DR, A. Effect of Rotor Blade Geometry on the Performance of Rotary-Winged Micro Air Vehicle. Defence Science Journal, [S. l.], v. 66, n. 6, p. 638–644, 2016. DOI: 10.14429/dsj.66.9659. Disponível em: https://publications.drdo.gov.in/ojs/index.php/dsj/article/view/9659. Acesso em: 15 jun. 2025.