Open access
Aug 2026
Simulation of aircraft unstable motions and unsteady aerodynamic testing with cable-driven parallel suspension system
This paper presents the development and experimental validation of a novel cable-driven parallel suspension mechanism (CDPSM) for investigating unstable, high-angle-of-attack aerodynamics in low-speed wind tunnel. Designed to overcome the limitations of conventional testing in simulating post-stall flight dynamics, the...
Xiao-Guang Wang, Xu Liu, Dongbo Han et al.
· Advances in Aerodynamics · 0 citations