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Euler-based throughflow method for inverse design and optimisation of turbomachinery blades

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Publication:1622191
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DOI10.1504/PCFD.2014.060138zbMath1400.76037OpenAlexW2025337426MaRDI QIDQ1622191

Simone Rosa Taddei, Francesco Larocc

Publication date: 12 November 2018

Published in: Progress in Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1504/pcfd.2014.060138


zbMATH Keywords

axisymmetric flow fieldblade forcesthroughflow surfaceturbomachinery blade inverse design


Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Finite volume methods applied to problems in fluid mechanics (76M12) General aerodynamics and subsonic flows (76G25)




Cites Work

  • Unnamed Item
  • A Contribution to the Numerical Prediction of Unsteady Flows
  • On the aerodynamic design of axial flow turbines by an implicit upwind axisymmetric method
  • An implicit form for the Osher upwind scheme
  • Euler-based inverse method for turbomachine blades. I - Two-dimensional cascades
  • An aerodynamic optimization method based on the inverse problem adjoint equations


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