scientific article; zbMATH DE number 1081095
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Publication:4362200
DOI<315::AID-FLD555>3.0.CO;2-L 10.1002/(SICI)1097-0363(19970815)25:3<315::AID-FLD555>3.0.CO;2-LzbMath0890.76060MaRDI QIDQ4362200
Patrick Queutey, Emmanuel Guilmineau, Jean Piquet
Publication date: 14 July 1998
Title: zbMATH Open Web Interface contents unavailable due to conflicting licenses.
hysteresis loopsforce coefficientsBaldwin-Barth modelCPI finite volume methoddeep dynamic stalldownstroke phaseK-omega SST modelpitching NACA 0012 aerofoilupstroke phase
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Related Items (3)
Applications of dynamic hybrid grid method for three-dimensional moving/deforming boundary problems ⋮ An implicit unfactored method for unsteady turbulent compressible flows with moving boundaries ⋮ Unsteady vorticity-streamfunction algorithm for external flows
Cites Work
- Solution of the implicitly discretized fluid flow equations by operator- splitting
- Incompressible flow calculations with a consistent physical interpolation finite volume approach
- Numerical study of the turbulent flow past an airfoil with trailing edge separation
- Navier-Stokes Solution of the Turbulent Flowfieid about an Isolated Airfoil
- A new fully coupled solution of the Navier‐Stokes equations
- Numerical prediction of dynamic forces on arbitrarily pitched airfoils
- Computation of unsteady laminar viscous flow past an aerofoil using the CPI method
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