The Effect of Turbulent Scales on Low-Pressure Turbine Aerodynamics: Part A: An Optimized Turbulent Boundary-Condition

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Autoren

  • Christoph Müller-Schindewolffs
  • Florian Herbst
Forschungs-netzwerk anzeigen

Details

OriginalspracheEnglisch
Titel des SammelwerksTurbo Expo
UntertitelPower for Land, Sea, and Air
Herausgeber (Verlag)American Society of Mechanical Engineers(ASME)
Seitenumfang16
ISBN (Print)9780791851005
PublikationsstatusVeröffentlicht - 2018
VeranstaltungASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition, GT 2018 - Oslo, Norwegen
Dauer: 11 Juni 201815 Juni 2018

Publikationsreihe

NameProceedings of the ASME Turbo Expo
Band2B-2018

Abstract

Exact inflow conditions for DNS and LES can be generated by resource-intensive precursor simulations of three-dimensional periodic boxes or infinite channels, in the case where a wallbounded flow is investigated. A cheaper and much more flexible alternative is the use of synthetic boundary conditions. In the proposed paper, a modified synthetic-eddy-method will be presented, which suits the demands and specifications of turbomachinery applications. It will further be extended to subsonic compressible flows by adding a mechanism to uncouple acoustic waves. It is applied to synthetically reproduce the wake of a turbine test case and validated against the original cascade simulation which is presented in the according Part B paper. This highly flexible approach also provides interfaces to prescribe unsteady inflow conditions, by temporally changing velocities, Reynolds stresses, and turbulent length-scales.

ASJC Scopus Sachgebiete

Zitieren

The Effect of Turbulent Scales on Low-Pressure Turbine Aerodynamics: Part A: An Optimized Turbulent Boundary-Condition . / Müller-Schindewolffs, Christoph; Herbst, Florian.
Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers(ASME), 2018. (Proceedings of the ASME Turbo Expo; Band 2B-2018).

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Müller-Schindewolffs, C & Herbst, F 2018, The Effect of Turbulent Scales on Low-Pressure Turbine Aerodynamics: Part A: An Optimized Turbulent Boundary-Condition . in Turbo Expo: Power for Land, Sea, and Air. Proceedings of the ASME Turbo Expo, Bd. 2B-2018, American Society of Mechanical Engineers(ASME), ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition, GT 2018, Oslo, Norwegen, 11 Juni 2018. https://doi.org/10.1115/GT2018-75162
Müller-Schindewolffs, C., & Herbst, F. (2018). The Effect of Turbulent Scales on Low-Pressure Turbine Aerodynamics: Part A: An Optimized Turbulent Boundary-Condition . In Turbo Expo: Power for Land, Sea, and Air (Proceedings of the ASME Turbo Expo; Band 2B-2018). American Society of Mechanical Engineers(ASME). https://doi.org/10.1115/GT2018-75162
Müller-Schindewolffs C, Herbst F. The Effect of Turbulent Scales on Low-Pressure Turbine Aerodynamics: Part A: An Optimized Turbulent Boundary-Condition . in Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers(ASME). 2018. (Proceedings of the ASME Turbo Expo). Epub 2018 Aug 30. doi: 10.1115/GT2018-75162
Müller-Schindewolffs, Christoph ; Herbst, Florian. / The Effect of Turbulent Scales on Low-Pressure Turbine Aerodynamics: Part A : An Optimized Turbulent Boundary-Condition . Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers(ASME), 2018. (Proceedings of the ASME Turbo Expo).
Download
@inproceedings{33548c4acf824333bf8d02a2979f9c3d,
title = "The Effect of Turbulent Scales on Low-Pressure Turbine Aerodynamics: Part A: An Optimized Turbulent Boundary-Condition ",
abstract = "Exact inflow conditions for DNS and LES can be generated by resource-intensive precursor simulations of three-dimensional periodic boxes or infinite channels, in the case where a wallbounded flow is investigated. A cheaper and much more flexible alternative is the use of synthetic boundary conditions. In the proposed paper, a modified synthetic-eddy-method will be presented, which suits the demands and specifications of turbomachinery applications. It will further be extended to subsonic compressible flows by adding a mechanism to uncouple acoustic waves. It is applied to synthetically reproduce the wake of a turbine test case and validated against the original cascade simulation which is presented in the according Part B paper. This highly flexible approach also provides interfaces to prescribe unsteady inflow conditions, by temporally changing velocities, Reynolds stresses, and turbulent length-scales.",
author = "Christoph M{\"u}ller-Schindewolffs and Florian Herbst",
year = "2018",
doi = "10.1115/GT2018-75162",
language = "English",
isbn = "9780791851005",
series = "Proceedings of the ASME Turbo Expo",
publisher = "American Society of Mechanical Engineers(ASME)",
booktitle = "Turbo Expo",
address = "United States",
note = "ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition, GT 2018 ; Conference date: 11-06-2018 Through 15-06-2018",

}

Download

TY - GEN

T1 - The Effect of Turbulent Scales on Low-Pressure Turbine Aerodynamics: Part A

T2 - ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition, GT 2018

AU - Müller-Schindewolffs, Christoph

AU - Herbst, Florian

PY - 2018

Y1 - 2018

N2 - Exact inflow conditions for DNS and LES can be generated by resource-intensive precursor simulations of three-dimensional periodic boxes or infinite channels, in the case where a wallbounded flow is investigated. A cheaper and much more flexible alternative is the use of synthetic boundary conditions. In the proposed paper, a modified synthetic-eddy-method will be presented, which suits the demands and specifications of turbomachinery applications. It will further be extended to subsonic compressible flows by adding a mechanism to uncouple acoustic waves. It is applied to synthetically reproduce the wake of a turbine test case and validated against the original cascade simulation which is presented in the according Part B paper. This highly flexible approach also provides interfaces to prescribe unsteady inflow conditions, by temporally changing velocities, Reynolds stresses, and turbulent length-scales.

AB - Exact inflow conditions for DNS and LES can be generated by resource-intensive precursor simulations of three-dimensional periodic boxes or infinite channels, in the case where a wallbounded flow is investigated. A cheaper and much more flexible alternative is the use of synthetic boundary conditions. In the proposed paper, a modified synthetic-eddy-method will be presented, which suits the demands and specifications of turbomachinery applications. It will further be extended to subsonic compressible flows by adding a mechanism to uncouple acoustic waves. It is applied to synthetically reproduce the wake of a turbine test case and validated against the original cascade simulation which is presented in the according Part B paper. This highly flexible approach also provides interfaces to prescribe unsteady inflow conditions, by temporally changing velocities, Reynolds stresses, and turbulent length-scales.

UR - http://www.scopus.com/inward/record.url?scp=85054096183&partnerID=8YFLogxK

U2 - 10.1115/GT2018-75162

DO - 10.1115/GT2018-75162

M3 - Conference contribution

AN - SCOPUS:85054096183

SN - 9780791851005

T3 - Proceedings of the ASME Turbo Expo

BT - Turbo Expo

PB - American Society of Mechanical Engineers(ASME)

Y2 - 11 June 2018 through 15 June 2018

ER -