A qualitative analysis of the flow inside the closed test section of the Politecnico di Milano large wind tunnel in presence of rotor effects has been carried out with the ROSITA RANS solver. The rotor is represented as an actuator disk. The analysis of the results of the performed steady state simulations allow for the determination of the flow breakdown boundaries in terms of tunnel operating parameters. Some indications are provided on experimental measurements which may be used for an on-line detection of the flow breakdown itself.

Computational Assessment of Flow Breakdown in Closed Section Model Rotor Tests

BIAVA, MASSIMO;VIGEVANO, LUIGI
2011-01-01

Abstract

A qualitative analysis of the flow inside the closed test section of the Politecnico di Milano large wind tunnel in presence of rotor effects has been carried out with the ROSITA RANS solver. The rotor is represented as an actuator disk. The analysis of the results of the performed steady state simulations allow for the determination of the flow breakdown boundaries in terms of tunnel operating parameters. Some indications are provided on experimental measurements which may be used for an on-line detection of the flow breakdown itself.
2011
37th European Rotorcraft Forum (ERF 2011)
9781618396266
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/603693
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