Numerical investigation of secondary flow and loss development in a low-pressure turbine cascade with divergent endwalls

Roberto Ciorciari; Tobias Schubert; Reinhard Niehuis

doi:10.29008/ETC2017-335

12^th European Conference on Turbomachinery Fluid dynamics & Thermodynamics

Paper ID:

ETC2017-335

Main Topic:

Axial Turbines

https://doi.org/10.29008/ETC2017-335

Authors

Roberto Ciorciari - Institute of Jet Propulsion, Universität der Bundeswehr München
Tobias Schubert - Institute of Jet Propulsion, Universität der Bundeswehr
Reinhard Niehuis - Institute of Jet Propulsion, Universität der Bundeswehr

Abstract

Secondary flow and loss development in the T106Div-EIZ LPT turbine cascade are investigated utilizing (U)RANS simulations in cases with and without periodically incoming wakes at Ma_2th = 0.59 and Re_2th = 2 · 10⁵. The predictions are compared to experimental data presented by Kirik and Niehuis (2015). The axial mid-span and overall loss development in the T106Div-EIZ and the T106A-EIZ in the steady case are analyzed regarding the effects caused by the different loading distributions and by the divergent endwall geometry. Furthermore, the entropy generation is analyzed in the T106Div-EIZ with periodical incoming wakes in several axial positions of interest and compared to the undisturbed steady case. It is found that in the front-loaded T106Div-EIZ, the incoming wakes cause a premature endwall loss production in the front part of the passage, resulting in a lower intensity of the secondary flow downstream and a redistribution of the loss generation components.