Aeroelastic tailoring analysis for advanced turbo propellers with composite blades

DOI10.1016/0045-7930(92)90023-OzbMath0825.76372OpenAlexW1967222676MaRDI QIDQ1198343

Takashi Yamane

Publication date: 16 January 1993

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7930(92)90023-o

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Composite and mixture properties (74E30) General aerodynamics and subsonic flows (76G25)

Related Items (1)

Influence of Fibre Orientation on the Dynamic Behaviour of Rotating Laminated Composite Blades

Uses Software

• Flutter

Cites Work

• Vibration analysis of composite turbopropellers using a nonlinear beam-type finite-element approach
• An improved two-node finite element for stability and natural frequencies of axial-loaded Timoshenko beams
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