Add to ORKGA 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
The majority of condition monitoring techniques employed today consider the acquisitioning and anal...
Experimental studies were carried out in the 0.6 m×0.6 m continuous transonic wind tunnel of CARDC i...
Experimental techniques to measure rotorcraft aerodynamic performance are widely used. However, most...
A qualitative analysis of the flow inside the closed test section of the Politecnico di Milano large...
A qualitative analysis of the flow inside the closed and open test sections of the Politecnico di Mi...
A systematic investigation into the design and simulation of flow parameters in a closed-loop wind t...
Ground based experiments are used to understand and measure rotor and airframe aerodynamic performan...
A methodology for numerically simulating the flow conditions in closed-circuit wind tunnels is devel...
This study presents an experimental and numerical investigation of the effects of tunnel blockage, d...
Aim of this paper is to provide a deep insight into the dynamic behavior of the flow through a Savon...
The present work applies a recently developed method1 to compute, by means of coupled CFD/CSD simula...
Mississippi State University has a subsonic closed return wind tunnel facility with an open test sec...
Geometrical wind-tunnel details can have a significant influence on the results of building aerodyna...
A detailed study of the air flow through the fan stage of a high bypass turbofan in engine-out condi...
The majority of condition monitoring techniques employed today consider the acquisitioning and anal...
Experimental studies were carried out in the 0.6 m×0.6 m continuous transonic wind tunnel of CARDC i...
Experimental techniques to measure rotorcraft aerodynamic performance are widely used. However, most...
A qualitative analysis of the flow inside the closed test section of the Politecnico di Milano large...
A qualitative analysis of the flow inside the closed and open test sections of the Politecnico di Mi...
A systematic investigation into the design and simulation of flow parameters in a closed-loop wind t...
Ground based experiments are used to understand and measure rotor and airframe aerodynamic performan...
A methodology for numerically simulating the flow conditions in closed-circuit wind tunnels is devel...
This study presents an experimental and numerical investigation of the effects of tunnel blockage, d...
Aim of this paper is to provide a deep insight into the dynamic behavior of the flow through a Savon...
The present work applies a recently developed method1 to compute, by means of coupled CFD/CSD simula...
Mississippi State University has a subsonic closed return wind tunnel facility with an open test sec...
Geometrical wind-tunnel details can have a significant influence on the results of building aerodyna...
A detailed study of the air flow through the fan stage of a high bypass turbofan in engine-out condi...
The majority of condition monitoring techniques employed today consider the acquisitioning and anal...
Experimental studies were carried out in the 0.6 m×0.6 m continuous transonic wind tunnel of CARDC i...
Experimental techniques to measure rotorcraft aerodynamic performance are widely used. However, most...