Comparison of turbine tip leakage flow for flat tip and squealer tip geometries at high-speed conditions

NL Key, T Arts - 2006 - asmedigitalcollection.asme.org
The tip leakage flow characteristics for flat and squealer turbine tip geometries are studied in
the von Karman Institute Isentropic Light Piston Compression Tube facility, CT-2, at different …

Convective heat transfer and aerodynamics in axial flow turbines

MG Dunn - Turbo Expo: Power for Land, Sea, and …, 2001 - asmedigitalcollection.asme.org
The primary focus of this paper is convective heat transfer in axial flow turbines. Research
activity involving heat transfer generally separates into two related areas: predictions and …

Analysis of DNS and LES of flow in a low pressure turbine cascade with incoming wakes and comparison with experiments

V Michelassi, J Wissink, W Rodi - Flow, turbulence and combustion, 2002 - Springer
The flow around a low-pressure turbine rotor blade with incoming periodic wakes is
computed by means of DNS and LES. The latter adopts a dynamic sub-grid-scale model …

Large-eddy simulation of flow around low-pressure turbine blade with incoming wakes

V Michelassi, JG Wissink, J Frohlich, W Rodi - AIAA journal, 2003 - arc.aiaa.org
THE high complexity of turbomachinery ows, which are threedimensional, unsteady, and
often transitional, requires powerful computational tools and models. In recent years …

Unsteady Flows and Component Interaction in Turbomachinery

S Salvadori, M Insinna, F Martelli - International Journal of …, 2024 - mdpi.com
Unsteady component interaction represents a crucial topic in turbomachinery design and
analysis. Combustor/turbine interaction is one of the most widely studied topics both using …

Thermal power plant upgrade via a rotating detonation combustor and retrofitted turbine with optimized endwalls

Z Liu, J Braun, G Paniagua - International Journal of Mechanical Sciences, 2020 - Elsevier
In the past decade, pressure gain combustion research has promised over 10 percentage-
points of increase in power plant thermal efficiency. Alas, to realize such potential gain, one …

Unsteady strong shock interactions in a transonic turbine: experimental and numerical analysis

G Paniagua, T Yasa, A de la Loma, L Castillon… - Journal of propulsion …, 2008 - arc.aiaa.org
IN HIGHLY loaded turbine stages, the nozzle guide vane (NGV) exit flow is often transonic.
The design of efficient turbines thus requires a thorough understanding of the unsteady …

Comparative study on steady and unsteady conjugate heat transfer analysis of a high pressure turbine blade

S Hwang, C Son, D Seo, DH Rhee, B Cha - Applied Thermal Engineering, 2016 - Elsevier
In this study, an analysis of steady-state and unsteady-state Conjugate Heat Transfer (CHT)
of an aeronautic high pressure gas turbine was conducted, which can calculate fluid and …

An investigation of the heat transfer and static pressure on the over-tip casing wall of an axial turbine operating at engine representative flow conditions.(II). Time …

SJ Thorpe, S Yoshino, RW Ainsworth… - International journal of …, 2004 - Elsevier
This article reports the measurements of time-resolved heat transfer rate and time-resolved
static pressure that have been made on the over-tip casing of a transonic axial-flow turbine …

Rotor-stator interactions in a four-stage low-speed axial compressor—Part I: Unsteady profile pressures and the effect of clocking

R Mailach, K Vogeler - J. Turbomach., 2004 - asmedigitalcollection.asme.org
This two-part paper presents detailed experimental investigations of unsteady aerodynamic
blade row interactions in the four-stage Low-Speed Research Compressor of Dresden. In …