Experimental investigation of the nonlinear aeroelastic response of spanwise-graded NACA 0012 wings under subsonic flow conditions
Published online on July 03, 2026
Abstract
Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications, Ahead of Print.
This study experimentally investigates the nonlinear aeroelastic response of three NACA 0012 wing configurations–Wing-Uniform (WU), Wing-Graded A (WG-A), and Wing-Graded B (WG-B)–distinguished by their spanwise mass distribution. The wings were fabricated ...
This study experimentally investigates the nonlinear aeroelastic response of three NACA 0012 wing configurations–Wing-Uniform (WU), Wing-Graded A (WG-A), and Wing-Graded B (WG-B)–distinguished by their spanwise mass distribution. The wings were fabricated ...