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Transition Location Effect on Shock Wave Boundary Layer Interaction, WP 3 Internal Flow Compressors

Hergt, Alexander and Grothe, Patrick and Flaszynski, Pawel and Szwaba, Ryszard and Piotrowicz, Michal and Kaczynski, Piotr and Tartinville, Benoit and Hirsch, Charles (2020) Transition Location Effect on Shock Wave Boundary Layer Interaction, WP 3 Internal Flow Compressors. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Designbook series (NNFM, volume 144) Springer Nature. pp. 229-296. ISBN 978-3-030-47460-7.

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Item URL in elib:https://elib.dlr.de/137310/
Document Type:Contribution to a Collection
Title:Transition Location Effect on Shock Wave Boundary Layer Interaction, WP 3 Internal Flow Compressors
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Hergt, Alexanderalexander.hergt (at) dlr.deUNSPECIFIED
Grothe, PatrickUNSPECIFIEDUNSPECIFIED
Flaszynski, PawelUNSPECIFIEDUNSPECIFIED
Szwaba, RyszardUNSPECIFIEDUNSPECIFIED
Piotrowicz, MichalUNSPECIFIEDUNSPECIFIED
Kaczynski, PiotrUNSPECIFIEDUNSPECIFIED
Tartinville, BenoitUNSPECIFIEDUNSPECIFIED
Hirsch, CharlesUNSPECIFIEDUNSPECIFIED
Date:July 2020
Journal or Publication Title:Notes on Numerical Fluid Mechanics and Multidisciplinary Designbook series (NNFM, volume 144)
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:144
Page Range:pp. 229-296
Publisher:Springer Nature
ISBN:978-3-030-47460-7
Status:Published
Keywords:transition, Shock wave-boundary-layer interaction
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:propulsion systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Fan and Compressor Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Hergt, Dr.-Ing. Alexander Silvio
Deposited On:10 Dec 2020 12:10
Last Modified:20 Jun 2021 15:54

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