
A comparison, between selected wind tunnel data from the NEW MEXICO measuring campaign and CFD computations are shown. The present work, documents that a state of the art CFD code, including a laminar turbulent transition model, can provide good agreement with experimental data. Good agreement is shown for the integral loads, radial distributions of blades forces, pressure distributions, and the velocity profiles up- and downstream of the rotor.
General fluid dynamics theory, simulation and other computational methods, CFD computations, wind tunnels, radial distributions, Mechanical components, wind tunnel, Turbulent flows, convection, and heat transfer, computational fluid dynamics, Flows in ducts, channels, and conduits, Fluid mechanics and aerodynamics (mechanical engineering), MEXICO rotor measurements, Applied fluid mechanics, rotors (mechanical), NEW MEXICO measuring campaign, blades, velocity profiles, CFD code, blades forces, laminar turbulent transition model, pressure distributions, laminar to turbulent transitions
General fluid dynamics theory, simulation and other computational methods, CFD computations, wind tunnels, radial distributions, Mechanical components, wind tunnel, Turbulent flows, convection, and heat transfer, computational fluid dynamics, Flows in ducts, channels, and conduits, Fluid mechanics and aerodynamics (mechanical engineering), MEXICO rotor measurements, Applied fluid mechanics, rotors (mechanical), NEW MEXICO measuring campaign, blades, velocity profiles, CFD code, blades forces, laminar turbulent transition model, pressure distributions, laminar to turbulent transitions
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