Evaluation AC6-14

From KBwiki
Jump to navigation Jump to search


Front Page

Description

Test Data

CFD Simulations

Evaluation

Best Practice Advice

Swirling flow in a conical diffuser generated with rotor-stator interaction

Application Challenge AC6-14   © copyright ERCOFTAC 2024

Comparison of Test Data and CFD

The mean velocity field is determined by time averaging over five complete runner revolutions for the hybrid models and eight complete runner revolutions for the URANS models to filter out all unsteadiness. The survey axes, \textit{S*}, at sections W0-W2 (see Fig. \ref{Test_rig}), are normalized by the throat radius, $R_{throat}$=0.05m, and the velocity is normalized by the bulk velocity at the throat, $W_{throat}$. The axial axis is downward and the runner rotates in the positive direction according to the right-hand rule.



Contributed by: A. Javadi, A. Bosioc, H Nilsson, S. Muntean, R. Susan-Resiga — Chalmers University of Technology

Front Page

Description

Test Data

CFD Simulations

Evaluation

Best Practice Advice


© copyright ERCOFTAC 2024