On the aerodynamic design of axial flow turbines by an implicit upwind axisymmetric method

DOI10.1080/17415971003686735zbMath1277.76035OpenAlexW2080068894MaRDI QIDQ3585361

Simone Rosa Taddei, Francesco Larocca

Publication date: 19 August 2010

Published in: Inverse Problems in Science and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/17415971003686735

zbMATH Keywords

implicit upwind schemeaxial flow turbine designaxisymmetric inverse methodEuler time-marching modelflux difference splitting operator

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Inverse problems for waves in solid mechanics (74J25) Numerical methods for inverse problems for initial value and initial-boundary value problems involving PDEs (65M32) Numerical methods for inverse problems for boundary value problems involving PDEs (65N21) Boundary value and inverse problems for harmonic functions in two dimensions (31A25)

Related Items (2)

Euler-based throughflow method for inverse design and optimisation of turbomachinery blades ⋮ Potential of specification of swirl in axisymmetric CFD methods for turbine blade aerodesign

Cites Work

• A nonreflecting outflow boundary condition for subsonic Navier-Stokes calculations
• Numerical Experiments with the Osher Upwind Scheme for the Euler Equations
• Euler equations - Implicit schemes and boundary conditions
• An implicit form for the Osher upwind scheme
• A design method for turbomachinery blading in three‐dimensional flow
• Euler-based inverse method for turbomachine blades. I - Two-dimensional cascades

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