Euler-based throughflow method for inverse design and optimisation of turbomachinery blades
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Publication:1622191
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
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
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- 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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