Volume 6C: Turbomachinery 2013
DOI: 10.1115/gt2013-95788
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Unsteady Flow Modeling Using Transient Rotor–Stator Interface

Abstract: Based on experimental investigation of unsteady flow phenomena in centrifugal compressor, conducted in LPI (SPbSPU), including the measurements of high frequency pressure and hot-wire probes, numerical calculation was conducted with the aid of commercial ANSYS CFX12. The object was a model of industrial compressor, tested in full range of mass flows (from maximum to the onset of surge). Unsteady turbulent flows were calculated with URANS, turbulence model - SST-Menter. Region between the impeller and diffuser … Show more

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“…The inlet boundary condition was the flow inlet, the flow rate was set to 10.66 m 3 /s, the outlet boundary condition was the pressure outlet, the pressure value was set to 1 atm, the solid wall was a non-slip wall, and the convergence accuracy was set to 1.0 × 10 −5 . The interface between the calculation domain of the impeller and the calculation domain of the inlet channel and the calculation domain of the guide vane body was set as the dynamic and static interface, and the Transient Rotor Stator interface type was used for the unsteady calculation [14,19,20]. The interface of another computing domain was set as the static interface, and the None interface model was adopted.…”
Section: Calculation Methods and Boundary Conditionsmentioning
confidence: 99%
“…The inlet boundary condition was the flow inlet, the flow rate was set to 10.66 m 3 /s, the outlet boundary condition was the pressure outlet, the pressure value was set to 1 atm, the solid wall was a non-slip wall, and the convergence accuracy was set to 1.0 × 10 −5 . The interface between the calculation domain of the impeller and the calculation domain of the inlet channel and the calculation domain of the guide vane body was set as the dynamic and static interface, and the Transient Rotor Stator interface type was used for the unsteady calculation [14,19,20]. The interface of another computing domain was set as the static interface, and the None interface model was adopted.…”
Section: Calculation Methods and Boundary Conditionsmentioning
confidence: 99%
“…The interfaces between impeller calculation domain and campaniform inlet conduit calculation domain and guide vane calculation domain are set as static and dynamic interface. Transient Rotor Stator interface type is used for unsteady calculation of pump device [19][20][21]. The interface between other calculation domains is set as static and static interface, and None interface model is used.…”
Section: Calculation Methods and Boundary Conditionsmentioning
confidence: 99%