A bifurcation method to calculate flutter characteristics of a helicopter having complex damping

DOI10.1016/0016-0032(75)90163-5zbMath0337.73040OpenAlexW2058796516MaRDI QIDQ1230541

Barry S. Thornton

Publication date: 1975

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0016-0032(75)90163-5

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Stability of dynamical problems in solid mechanics (74H55)

Cites Work

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• On difference differential equations with periodic coefficients
• Bending-torsional flutter of a cantilevered wing containing a tip mass and subjected to a transverse follower force
• Damping loss in a cascade of fluttering phased aerofoils

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