High-Fidelity Framework for Fluid–Structure Interaction Analysis of Jet-Engine Turbine Blades Under Vibratory Loading. Acceleron Aerospace Journal, [S. l.], v. 6, n. 1, p. 1682–1695, 2026. DOI: 10.61359/11.2106-2605. Disponível em: https://www.acceleron.org.in/index.php/aaj/article/view/262. Acesso em: 30 mar. 2026.