Recommendations for achieving accurate numerical simulation of tip clearance flows in transonic compressor rotors

DE Van Zante, AJ Strazisar, JR Wood… - J …, 2000 - asmedigitalcollection.asme.org
The tip clearance flows of transonic compressor rotors are important because they have a
significant impact on rotor and stage performance. A wall-bounded shear layer formed by …

A numerical investigation of the influence of casing treatments on the tip leakage flow in a HPC front stage

I Wilke, HP Kau - Turbo Expo: Power for Land, Sea …, 2002 - asmedigitalcollection.asme.org
This paper describes the influence of casing treatments on the tip leakage flow and its
resulting vortex. The presented results and conclusions are based on steady state numerical …

A numerical investigation of the flow mechanisms in a high pressure compressor front stage with axial slots

I Wilke, HP Kau - J. Turbomach., 2004 - asmedigitalcollection.asme.org
This paper describes the impact of axial slots on the flow field in a transonic rotor blade row.
The presented results are completely based on time-accurate three-dimensional numerical …

Optimization of organic Rankine cycle power systems considering multistage axial turbine design

A Meroni, JG Andreasen, G Persico, F Haglind - Applied Energy, 2018 - Elsevier
Organic Rankine cycle power systems represent a viable and efficient solution for the
exploitation of medium-to-low temperature heat sources. Despite the large number of …

Numerical investigation of casing treatment mechanisms with a conservative mixed-cell approach

H Yang, D Nuernberger… - … Expo: Power for …, 2003 - asmedigitalcollection.asme.org
A conservative mixed-cell approach of second-order accuracy is presented and applied to
investigate the mechanisms of a self-recirculating casing treatment coupled with a transonic …

Numerically aided design of a high-efficient casing treatment for a transonic compressor

I Wilke, HP Kau, G Brignole - … Expo: Power for …, 2005 - asmedigitalcollection.asme.org
The transonic NASA Rotor 37 is well known for the occurrence of rotating stall at operation
points close to stall. Several experimental and numerical investigations have shown that the …

A numerical investigation of the flow mechanisms in a HPC front stage with axial slots

I Wilke, HP Kau - Turbo Expo: Power for Land, Sea …, 2003 - asmedigitalcollection.asme.org
This paper describes the impact of axial slots on the flow field in a transonic rotor blade row.
The presented results are completely based on time-accurate 3-dimensional numerical …

Experimental and numerical analysis of axial skewed slot casing treatments for a transonic compressor stage

FCT Danner, HP Kau… - … Expo: Power for …, 2009 - asmedigitalcollection.asme.org
An investigation of a single-stage transonic compressor with axial skewed slot casing
treatments is presented. The studied compressor stage is characterised by a design mass …

Multistage three-dimensional Navier-Stokes computation of off-design operation of a four-stage turbine

GA Gerolymos, C Hanisch - … , Part A: Journal of Power and …, 1999 - journals.sagepub.com
In this paper a three-dimensional computational methodology for multistage turbomachinery
flows is developed, validated and applied in analysing the reduced mass flowrate operation …

Recommendations for achieving accurate numerical simulation of tip clearance flows in transonic compressor rotors

DE Van Zante, AJ Strazisar… - … Expo: Power for …, 1999 - asmedigitalcollection.asme.org
The tip clearance flows of transonic compressor rotors are important because they have a
significant impact on rotor and stage performance. While numerical simulations of these …