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

DOI10.1017/s1446181123000081zbMath1523.76055OpenAlexW4384558850MaRDI QIDQ6057860

Michael H. Meylan, Benjamin Maldon

Publication date: 5 October 2023

Published in: The ANZIAM Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/s1446181123000081

zbMATH Keywords

lift dissymmetrymaximum speed thresholdminimum rotor angular velocity

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) General theory of rotating fluids (76U05)

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Cites Work

• Helicopter blade flapping with and without small angle assumption in the presence of dynamic stall
• Effect of the wing shape on the thrust of flapping wing
• On the flapping motion of a helicopter blade

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