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Multidisciplinary optimization of propeller blades: Focus on the aeroelastic results

  • B. G. Marinus
  • , R. A. van den Braembussche
  • , W. Bosschaerts
  • , M. Roger
  • Karman Institute for Fluid Dynamics
  • Ecole Centrale de Lyon

Onderzoeksoutput: Hoofdstuk in Boek/Rapport/CongresprocedureConferentiebijdragepeer review

3 Citaten (Scopus)

Samenvatting

Concurrent aerodynamic, aeroacoustic and aeroelastic optimization of transonic propeller blades is performed with a Multi-Objective Differential Evolution technique. The optimization process relies on a metamodel to deliver performance estimates as well as on recurrent Computational Fluid Dynamics, Computational Hybrid Aeroacoustics and Computational Structural Mechanics simulations in order to safeguard the accuracy. The innovative design parameters for the radial distributions of sweep, twist, chord and thickness as well as for the shape of the two airfoil sections used to manufacture the blade, consist in the control points of a b-spline parameterization of these curves. The optimization results are discussed in terms of aerodynamic and aeroelastic performances with a limited discussion of the aeroacoustic behavior.

Originele taal-2Engels
Titel47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011
UitgeverijAmerican Institute of Aeronautics and Astronautics Inc
ISBN van geprinte versie9781600869495
DOI's
StatusGepubliceerd - 2011
Evenement47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 - San Diego, CA, Verenigde Staten van Amerika
Duur: 31 jul. 20113 aug. 2011

Publicatie series

Naam47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011

Congres

Congres47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011
Land/RegioVerenigde Staten van Amerika
StadSan Diego, CA
Periode31/07/113/08/11

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