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Aeroelastic Testcases in IDIHOM Project

  • K. Kotecki
  • H. van der Ven
  • J. Kok
  • H. Hausa
  • M. Nowak
  • W. Stankiewicz
  • R. Roszak
  • M. Morzyński
Part of the Notes on Numerical Fluid Mechanics and Multidisciplinary Design book series (NNFM, volume 128)

Abstract

In the IDIHOM Project three aeroelastic testcases have been calculated. Two of them - LANN Wing and DLR-F6 wing-body configuration - have been conducted by PUT. The last one, the HART II rotor has been prepared by NLR. Each partner has used different technology and software tools, hence each of the testcases describes the results of the simulation and technology which has been used.

Keywords

Aeroelasticisty high order CFD 

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Copyright information

© Springer International Publishing Switzerland 2015

Authors and Affiliations

  • K. Kotecki
    • 1
  • H. van der Ven
    • 2
  • J. Kok
    • 2
  • H. Hausa
    • 1
  • M. Nowak
    • 1
  • W. Stankiewicz
    • 1
  • R. Roszak
    • 1
  • M. Morzyński
    • 1
  1. 1.Division of Virtual EngineeringPoznań University of TechnologyPoznańPoland
  2. 2.Netherlands National Aerospace Laboratory, Flight Physics and LoadsAmsterdamThe Netherlands

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