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Heat transfer amplification in transitional shock-wave/boundary-layer interactions

Lunte, Jens and Schülein, Erich (2019) Heat transfer amplification in transitional shock-wave/boundary-layer interactions. In: AIAA Aviation 2019. AIAA Aviation 2019, 17.-21. Juni 2019, Dallas, Texas, USA.

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Official URL: https://www.aiaa.org/aviation


Heat flux measurements of transitional shock-wave/boundary-layer interactions (SWBLI) were conducted by quantitative infrared thermography. The shock intensity and mutual position of the impingement and transition locations were varied independently. The shock induced Stanton number peaks are maximal for transitional SWBLI and stronger shocks cause higher heat transfer amplification. The highest amplification rates for each shock intensity depend on the transitional state at the impingement location. Weaker shocks require a further developed transitional state at the impingement location for the highest amplification due to less shock induced turbulence. Numerical simulations with the DLR TAU-Code were conducted for the limiting boundary layer cases (laminar & turbulent) and cover the entire experimental parameter study.

Item URL in elib:https://elib.dlr.de/123337/
Document Type:Conference or Workshop Item (Speech)
Title:Heat transfer amplification in transitional shock-wave/boundary-layer interactions
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Lunte, JensJens.lunte (at) dlr.deUNSPECIFIED
Schülein, ErichErich.Schuelein (at) dlr.dehttps://orcid.org/0000-0002-1125-8504
Date:June 2019
Journal or Publication Title:AIAA Aviation 2019
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
EditorsEmailEditor's ORCID iD
Keywords:Heat transfer amplifications, SWBLI, Mach 6
Event Title:AIAA Aviation 2019
Event Location:Dallas, Texas, USA
Event Type:international Conference
Event Dates:17.-21. Juni 2019
Organizer:American Institute of Aeronautics and Astronautics
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 - Military Technologies (old)
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > High Speed Configurations, GO
Deposited By: Lunte, Jens
Deposited On:25 Jun 2019 13:51
Last Modified:01 Jul 2020 03:00

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