Aeroelastic tailoring using lamination parameters

DOI10.1007/s00158-009-0437-6zbMath1274.76001OpenAlexW1528218289MaRDI QIDQ381477

Glenn A. A. Thuwis, Roeland de Breuker, Zafer Gürdal, Mostafa M. Abdalla

Publication date: 15 November 2013

Published in: Structural and Multidisciplinary Optimization (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00158-009-0437-6

zbMATH Keywords

drag reduction\texttt{NASTRAN}\texttt{VSAERO}aeroelastic tailoringautomotivelamination parameters

Mathematics Subject Classification ID

Software, source code, etc. for problems pertaining to fluid mechanics (76-04)

Uses Software

• NASTRAN
• SIMPACK
• VSAERO
• ModelCenter
• DistMesh

Cites Work

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• Review of coupling methods for non-matching meshes
• Piecewise polynomial, positive definite and compactly supported radial functions of minimal degree
• Multivariate interpolation for fluid-structure-interaction problems using radial basis functions
• Unified fluid–structure interpolation and mesh motion using radial basis functions
• In-plane response of laminates with spatially varying fiber orientations - Variable stiffness concept
• Coupling fluid (CFD) and structural (FE) models using finite interpolation elements
• A Simple Mesh Generator in MATLAB
• AERODYNAMICS OF RACE CARS
• A modern course in aeroelasticity.

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