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Quantitative determination of the intermittency factor in a transitional Mach 6 flat plate boundary layer using three independent measurement methods

Lunte, Jens and Schülein, Erich (2023) Quantitative determination of the intermittency factor in a transitional Mach 6 flat plate boundary layer using three independent measurement methods. In: 2nd European Symposium on Laminar/Turbulent Transition in Hypersonic Regime. 2nd European Symposium on Laminar/Turbulent Transition in Hypersonic Regime, 2023-10-04 - 2023-10-06, Bordeaux, Frankreich.

Full text not available from this repository.

Official URL: https://www.hyfar-ara.org/en/hypersonic-transition-2023-old/#top


Item URL in elib:https://elib.dlr.de/198811/
Document Type:Conference or Workshop Item (Speech)
Title:Quantitative determination of the intermittency factor in a transitional Mach 6 flat plate boundary layer using three independent measurement methods
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Lunte, JensUNSPECIFIEDhttps://orcid.org/0000-0002-0755-0166UNSPECIFIED
Schülein, ErichUNSPECIFIEDhttps://orcid.org/0000-0002-1125-8504UNSPECIFIED
Date:October 2023
Journal or Publication Title:2nd European Symposium on Laminar/Turbulent Transition in Hypersonic Regime
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
UNSPECIFIEDHYFAR-ARAUNSPECIFIEDUNSPECIFIED
Status:Published
Keywords:transition; hypersonic; intermittency; Mach 6; FLDI; PCB; Stanton number; QIRT; flat plate
Event Title:2nd European Symposium on Laminar/Turbulent Transition in Hypersonic Regime
Event Location:Bordeaux, Frankreich
Event Type:international Conference
Event Start Date:4 October 2023
Event End Date:6 October 2023
Organizer:HYFAR-ARA
HGF - Research field:other
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L DT - Defense Technology
DLR - Research theme (Project):L - Effect
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > High Speed Configurations, GO
Deposited By: Lunte, Jens
Deposited On:30 Nov 2023 15:44
Last Modified:24 Apr 2024 20:59

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