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An aeroelastic model for composite rotor blades with straight and swept tips. I: Eroelastic stability in hover

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Publication:872857
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DOI10.1016/S0020-7462(01)00109-3zbMath1346.74019MaRDI QIDQ872857

Marino De Terlizzi, Kuo-An Yuan, Peretz P. Friedmann

Publication date: 28 March 2007

Published in: International Journal of Non-Linear Mechanics (Search for Journal in Brave)



Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Plastic materials, materials of stress-rate and internal-variable type (74C99)


Related Items (2)

Finite element linear and nonlinear, static and dynamic analysis of structural elements, an addendum ⋮ A moderate deflection composite helicopter rotor blade model with an improved cross-sectional analysis




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