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BOUNDARY LAYER ANALYSIS OF A TRANSONIC HIGH-PRESSURE TURBINE VANE USING ULTRA-FAST-RESPONSE TEMPERATURE-SENSITIVE PAINT

Petersen, Anna and Hilfer, Michael (2023) BOUNDARY LAYER ANALYSIS OF A TRANSONIC HIGH-PRESSURE TURBINE VANE USING ULTRA-FAST-RESPONSE TEMPERATURE-SENSITIVE PAINT. ASME Turbo Expo 2023, 2023-06-26 - 2023-06-30, Boston. doi: 10.1115/GT2023-101889.

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Item URL in elib:https://elib.dlr.de/195851/
Document Type:Conference or Workshop Item (Speech)
Additional Information:GT2023-101889
Title:BOUNDARY LAYER ANALYSIS OF A TRANSONIC HIGH-PRESSURE TURBINE VANE USING ULTRA-FAST-RESPONSE TEMPERATURE-SENSITIVE PAINT
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Petersen, AnnaUNSPECIFIEDhttps://orcid.org/0000-0003-4819-4994UNSPECIFIED
Hilfer, MichaelUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:26 June 2023
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI:10.1115/GT2023-101889
Status:Published
Keywords:HPT-NGV Turbine iTSP Cascade EGG Transition
Event Title:ASME Turbo Expo 2023
Event Location:Boston
Event Type:international Conference
Event Start Date:26 June 2023
Event End Date:30 June 2023
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Advanced Materials and New Manufacturing Technologies
Location: Göttingen
Institutes and Institutions:Institute of Propulsion Technology > Turbine
Institute for Aerodynamics and Flow Technology > Experimental Methods, GO
Deposited By: Petersen, Anna
Deposited On:10 Jul 2023 08:59
Last Modified:27 May 2024 13:36

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