Influence of Transonic Flow on the Tip-Leakage Vortex in a Turbine Cascade

Research output: Contribution to conferencePaperResearch

Authors

View graph of relations

Details

Original languageEnglish
Publication statusPublished - Nov 2019
EventInternational Gas Turbine Congress (IGTC) 2019 - Toranomon Hills Forum, Tokyo, Japan
Duration: 17 Nov 201922 Nov 2019

Conference

ConferenceInternational Gas Turbine Congress (IGTC) 2019
Country/TerritoryJapan
Period17 Nov 201922 Nov 2019

Abstract

In this paper we analyse numerically how the tip-leakage vortex in a linear cascade is impacted by transonic flow in general and by compression shocks in particular. We show that, despite higher blade loading and consequently stronger tip-leakage vortices, the axial-momentum deficit in the tip region decreases for transonic flow conditions. In addition, the overturning induced by the tip-leakage vortex decreases for transonic flow conditions. Both effects can be regarded as highly favourable when the potential reduction in boundary-layer separation in downstream diffusers or intermediate ducts is considered.

Cite this

Influence of Transonic Flow on the Tip-Leakage Vortex in a Turbine Cascade. / Mimic, Dajan; Herbst, Florian.
2019. Paper presented at International Gas Turbine Congress (IGTC) 2019, Japan.

Research output: Contribution to conferencePaperResearch

Mimic D, Herbst F. Influence of Transonic Flow on the Tip-Leakage Vortex in a Turbine Cascade. 2019. Paper presented at International Gas Turbine Congress (IGTC) 2019, Japan.
Mimic, Dajan ; Herbst, Florian. / Influence of Transonic Flow on the Tip-Leakage Vortex in a Turbine Cascade. Paper presented at International Gas Turbine Congress (IGTC) 2019, Japan.
Download
@conference{c8db4a7867934a1ba0d520f9952e4dc0,
title = "Influence of Transonic Flow on the Tip-Leakage Vortex in a Turbine Cascade",
abstract = "In this paper we analyse numerically how the tip-leakage vortex in a linear cascade is impacted by transonic flow in general and by compression shocks in particular. We show that, despite higher blade loading and consequently stronger tip-leakage vortices, the axial-momentum deficit in the tip region decreases for transonic flow conditions. In addition, the overturning induced by the tip-leakage vortex decreases for transonic flow conditions. Both effects can be regarded as highly favourable when the potential reduction in boundary-layer separation in downstream diffusers or intermediate ducts is considered.",
author = "Dajan Mimic and Florian Herbst",
year = "2019",
month = nov,
language = "English",
note = "International Gas Turbine Congress (IGTC) 2019 ; Conference date: 17-11-2019 Through 22-11-2019",

}

Download

TY - CONF

T1 - Influence of Transonic Flow on the Tip-Leakage Vortex in a Turbine Cascade

AU - Mimic, Dajan

AU - Herbst, Florian

PY - 2019/11

Y1 - 2019/11

N2 - In this paper we analyse numerically how the tip-leakage vortex in a linear cascade is impacted by transonic flow in general and by compression shocks in particular. We show that, despite higher blade loading and consequently stronger tip-leakage vortices, the axial-momentum deficit in the tip region decreases for transonic flow conditions. In addition, the overturning induced by the tip-leakage vortex decreases for transonic flow conditions. Both effects can be regarded as highly favourable when the potential reduction in boundary-layer separation in downstream diffusers or intermediate ducts is considered.

AB - In this paper we analyse numerically how the tip-leakage vortex in a linear cascade is impacted by transonic flow in general and by compression shocks in particular. We show that, despite higher blade loading and consequently stronger tip-leakage vortices, the axial-momentum deficit in the tip region decreases for transonic flow conditions. In addition, the overturning induced by the tip-leakage vortex decreases for transonic flow conditions. Both effects can be regarded as highly favourable when the potential reduction in boundary-layer separation in downstream diffusers or intermediate ducts is considered.

M3 - Paper

T2 - International Gas Turbine Congress (IGTC) 2019

Y2 - 17 November 2019 through 22 November 2019

ER -

By the same author(s)