COUPLED SIMULATION OF A SHROUDED TURBINE BLADE ROW WITH CONTACT FRICTION INTERFACES - ANALYSIS OF A LIMIT TORUS OSCILLATION

Berthold, Christian and Frey, Christian (2022) COUPLED SIMULATION OF A SHROUDED TURBINE BLADE ROW WITH CONTACT FRICTION INTERFACES - ANALYSIS OF A LIMIT TORUS OSCILLATION. Proceedings of 16th International Symposium on Unsteady Aerodynamics, Aeroacoustics & Aeroelasticity of Turbomachines, 2022-09-19 - 2022-09-23, Toledo.

PDF
530kB

Item URL in elib:

https://elib.dlr.de/189609/

Document Type:

Conference or Workshop Item (Speech)

Title:

COUPLED SIMULATION OF A SHROUDED TURBINE BLADE ROW WITH CONTACT FRICTION INTERFACES - ANALYSIS OF A LIMIT TORUS OSCILLATION

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Berthold, Christian	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Frey, Christian	UNSPECIFIED	https://orcid.org/0000-0003-0496-9225	UNSPECIFIED

Date:

2022

Refereed publication:

Open Access:

Yes

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Accepted

Keywords:

Flutter, Aeroelasticity, Limit Torus Oscillation, Friction, Nonlinear

Event Title:

Proceedings of 16th International Symposium on Unsteady Aerodynamics, Aeroacoustics & Aeroelasticity of Turbomachines

Event Location:

Toledo

Event Type:

international Conference

Event Start Date:

19 September 2022

Event End Date:

23 September 2022

Organizer:

ISUAAAT

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Aeronautics

HGF - Program Themes:

Clean Propulsion

DLR - Research area:

Aeronautics

DLR - Program:

L CP - Clean Propulsion

DLR - Research theme (Project):

L - Virtual Engine

Location:

Köln-Porz

Institutes and Institutions:

Institute of Propulsion Technology

Deposited By:

Berthold, Christian

Deposited On:

17 Nov 2022 11:16

Last Modified:

24 Apr 2024 20:50

Repository Staff Only: item control page