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Numerical investigations of rotational effects on boundary-layer instabilities on the Z49 open rotor model

Theiß, Alexander and Hein, Stefan and Pascal, Lucas and Julien, Cliquet (2022) Numerical investigations of rotational effects on boundary-layer instabilities on the Z49 open rotor model. In: AIAA SciTech 2022 Forum, pp. 1-16. ARC. AIAA Scitech Forum 2022, 2022-01-03 - 2022-01-07, San Diego, USA. doi: 10.2514/6.2022-2541. ISBN 978-162410631-6.

Full text not available from this repository.

Official URL: https://doi.org/10.2514/6.2022-2541

Abstract

Spatial linear stability analyses are performed in order to study laminar-turbulent transition in the boundary layer on the Z49 rotor, rotating in a Ma = 0.75 freestream. In a rotating reference frame, terms corresponding to Coriolis and centrifugal forces appear in the linearized disturbance equations. However, the effect of these rotational terms on the stability of laminar boundary layers is only partially understood. The rotational terms' impact on the transition mechanisms is studied by neglecting or considering rotation in the linear local stability and parabolized stability equations. The present results show that rotation hardly affects the instability characteristics of Tollmien-Schlichting waves. On the other hand, rotation destabilizes the cross-flow instabilities, but not enough to trigger cross-flow-dominated transition at the investigated operating condition.

Item URL in elib:https://elib.dlr.de/142494/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA 2022-2541 Session: Instability and Transition X
Title:Numerical investigations of rotational effects on boundary-layer instabilities on the Z49 open rotor model
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Theiß, AlexanderUNSPECIFIEDhttps://orcid.org/0000-0003-4034-3246UNSPECIFIED
Hein, StefanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Pascal, LucasOneraUNSPECIFIEDUNSPECIFIED
Julien, CliquetAirbusUNSPECIFIEDUNSPECIFIED
Date:January 2022
Journal or Publication Title:AIAA SciTech 2022 Forum
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.2514/6.2022-2541
Page Range:pp. 1-16
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
UNSPECIFIEDAIAAUNSPECIFIEDUNSPECIFIED
Publisher:ARC
ISBN:978-162410631-6
Status:Published
Keywords:Laminar-turbulent transition, Linear stability theory, Parabolized stability equations, Rotational effects
Event Title:AIAA Scitech Forum 2022
Event Location:San Diego, USA
Event Type:international Conference
Event Start Date:3 January 2022
Event End Date:7 January 2022
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Digital Technologies, L - Virtual Aircraft and  Validation
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > High Speed Configurations, GO
Deposited By: Theiß, Alexander
Deposited On:01 Feb 2022 12:41
Last Modified:24 Apr 2024 20:42

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