On the flapping motion of a helicopter blade

DOI10.1016/J.APM.2017.01.055zbMath1443.76062OpenAlexW2580159000MaRDI QIDQ2281886

Fu-Shang Wei, Oscar M. Perdomo

Publication date: 6 January 2020

Published in: Applied Mathematical Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.apm.2017.01.055

zbMATH Keywords

periodic solutionshelicopter vibrationblade flapping motionrotor blade design

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Mathematical modeling or simulation for problems pertaining to fluid mechanics (76-10)

Related Items (1)

FLIGHT LIMITATIONS IMPOSED ON SINGLE ROTOR AND COAXIAL HELICOPTERS BY THE LIFT EQUATION

Cites Work

• Helicopter blade flapping with and without small angle assumption in the presence of dynamic stall

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