The article aims to determine the effect of reverse flow on the damping, frequency, and the stability boundaries of helicopter rotor-blade flapping dynamics and to investigate the behavior of the system in the limit of small Lock number and small advance ratio. The system is represented by a linear ordinary differential equation that gives results resembling to experimental data.
Mechanical Engineering and Material Sciences Independent Study
Date of Submission
Gao, Yunfei, "Response of Rotor Blade Flapping in Forward Flight" (2022). Mechanical Engineering and Materials Science Independent Study. 216.