Structural and Multidisciplinary Optimization

, Volume 41, Issue 4, pp 637–646

Aeroelastic tailoring using lamination parameters

Drag reduction of a Formula One rear wing
  • Glenn A. A. Thuwis
  • Roeland De Breuker
  • Mostafa M. Abdalla
  • Zafer Gürdal
Open Access
Industrial Application

DOI: 10.1007/s00158-009-0437-6

Cite this article as:
Thuwis, G.A.A., De Breuker, R., Abdalla, M.M. et al. Struct Multidisc Optim (2010) 41: 637. doi:10.1007/s00158-009-0437-6

Abstract

The aim of the present work is to passively reduce the induced drag of the rear wing of a Formula One car at high velocity through aeroelastic tailoring. The angle-of-attack of the rear wing is fixed and is determined by the required downforce needed to get around a turn. As a result, at higher velocity, the amount of downforce and related induced drag increases. The maximum speed on a straight part is thus reduced due to the increase in induced drag. A fibre reinforced composite torsion box with extension-shear coupled upper and lower skins is used leading to bending-torsion coupling. Three-dimensional static aeroelastic analysis is performed loosely coupling the Finite Element code Nastran and the Computational Fluid Dynamics panel code VSAERO using ModelCenter. A wing representative of Formula One rear wings is optimised for minimum induced drag using a response surface methodology. Results indicate that a substantial induced drag reduction is achievable while maintaining the desired downforce during low speed turns.

Keywords

Aeroelastic tailoring Lamination parameters Drag reduction Automotive 

Copyright information

© The Author(s) 2009

Authors and Affiliations

  • Glenn A. A. Thuwis
    • 1
  • Roeland De Breuker
    • 1
  • Mostafa M. Abdalla
    • 1
  • Zafer Gürdal
    • 1
  1. 1.Faculty of Aerospace EngineeringTU DelftHS DelftThe Netherlands

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