Abstract
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.
Document Type
Final Report
Class Name
Mechanical Engineering and Material Sciences Independent Study
Date of Submission
12-9-2022
Recommended Citation
Gao, Yunfei, "Response of Rotor Blade Flapping in Forward Flight" (2022). Mechanical Engineering and Materials Science Independent Study. 216.
https://openscholarship.wustl.edu/mems500/216
COinS