Structural optimization of an aeroelastically tailored composite flat plate made of woven fiberglass/epoxy

DOI10.1007/S00707-007-0488-YzbMath1139.74044OpenAlexW2097672765MaRDI QIDQ932001

D. L. Majid, Shahnor Basri, A. S. Mohd Rafie, E. J. Abdullah, A. Attaran

Publication date: 8 July 2008

Published in: Acta Mechanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00707-007-0488-y

zbMATH Keywords

surface splinesmodal approachdoublet-lattice method

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Plates (74K20) Composite and mixture properties (74E30) Optimization of other properties in solid mechanics (74P10)

Related Items (1)

Comparative study of recent metaheuristics for solving a multiobjective transonic aeroelastic optimization of a composite wing

Uses Software

• NASTRAN
• PROMAL

Cites Work

• On the aeroelastic instability of two-dimensional panels in uniform incompressible flow
• Aeroelastic instability and response of advanced aircraft wings at subsonic flight speeds
• A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.
• Unnamed Item

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