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The Present Challenge of Transonic Compressor Blade Design

Hergt, Alexander and Klinner, Joachim and Wellner, Jens and Willert, Christian and Grund, Sebastian and Steinert, Wolfgang and Beversdorff, Manfred (2019) The Present Challenge of Transonic Compressor Blade Design. ASME Journal of Turbomachinery, 141 (9), 091004. American Society of Mechanical Engineers (ASME). doi: 10.1115/1.4043329. ISSN 0889-504X.

Full text not available from this repository.

Official URL: https://doi.org/10.1115/1.4043329

Item URL in elib:https://elib.dlr.de/129902/
Document Type:Article
Title:The Present Challenge of Transonic Compressor Blade Design
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Hergt, Alexanderalexander.hergt (at) dlr.deUNSPECIFIED
Klinner, JoachimJoachim.Klinner (at) dlr.dehttps://orcid.org/0000-0003-2709-9664
Wellner, Jensjens.wellner (at) dlr.deUNSPECIFIED
Willert, ChristianChris.Willert (at) dlr.dehttps://orcid.org/0000-0002-1668-0181
Grund, Sebastiansebastian.grund (at) dlr.deUNSPECIFIED
Steinert, Wolfgangwolfgang.steinert (at) dlr.deUNSPECIFIED
Beversdorff, ManfredManfred.Beversdorff (at) dlr.deUNSPECIFIED
Date:September 2019
Journal or Publication Title:ASME Journal of Turbomachinery
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:Yes
DOI :10.1115/1.4043329
Page Range:091004
Publisher:American Society of Mechanical Engineers (ASME)
Keywords:Transonic Cascade Shock 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
Institute of Propulsion Technology > Engine Measurement Systems
Institute of Propulsion Technology > Fan and Compressor
Deposited By: Hergt, Dr.-Ing. Alexander Silvio
Deposited On:28 Oct 2019 10:31
Last Modified:20 Jun 2021 15:52

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