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Adaptive harmonic linearized Navier-Stokes equations used for boundary-layer instability analysis in the presence of large streamwise gradients.

Franco, Juan Alberto and Hein, Stefan (2018) Adaptive harmonic linearized Navier-Stokes equations used for boundary-layer instability analysis in the presence of large streamwise gradients. In: AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting, 210059. AIAA Scitech 2018, 8.-12. Jan. 2018, Gaylord Palms, Kissimmee, Florida, USA. DOI: 10.2514/6.2018-1540 ISBN 978-162410524-1

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Official URL: https://arc.aiaa.org/doi/10.2514/6.2018-1540


Item URL in elib:https://elib.dlr.de/119474/
Document Type:Conference or Workshop Item (Speech)
Title:Adaptive harmonic linearized Navier-Stokes equations used for boundary-layer instability analysis in the presence of large streamwise gradients.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Franco, Juan Albertojuan.franco (at) dlr.deUNSPECIFIED
Hein, Stefanstefan.hein (at) dlr.deUNSPECIFIED
Date:January 2018
Journal or Publication Title:AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:210059
DOI :10.2514/6.2018-1540
Editors:
EditorsEmail
UNSPECIFIEDAIAA
ISBN:978-162410524-1
Status:Published
Keywords:Boundary-layer laminar turbulent transition, surface irregularities, AHLNS
Event Title:AIAA Scitech 2018
Event Location:Gaylord Palms, Kissimmee, Florida, USA
Event Type:international Conference
Event Dates:8.-12. Jan. 2018
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > High Speed Configurations, GO
Deposited By: Franco, Juan
Deposited On:15 May 2018 11:56
Last Modified:09 Jan 2019 08:23

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