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Development of a Highly Sensitive Temperature-Sensitive Paint for Measurements under Cryogenic Temperatures (100 – 160 K) Conditions

Klein, Christian and Henne, Ulrich and Costantini, Marco and Ondrus, Vladimir and Beifuss, Uwe (2016) Development of a Highly Sensitive Temperature-Sensitive Paint for Measurements under Cryogenic Temperatures (100 – 160 K) Conditions. AIAA SciTech 2016 - 54th AIAA Aerospace Sciences Meeting, 2016-01-04 - 2016-01-08, San Diego, CA, USA. doi: 10.2514/6.2016-0650.

Full text not available from this repository.

Official URL: http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0650

Abstract

A new temperature-sensitive paint (TSP) was developed to capture images with high signal-to-noise ratio in wind tunnel tests under cryogenic temperature (100 – 160 K) conditions. Typical applications of TSP are the detection of boundary-layer transition and the measurement of the temperature distribution on the model surface. Conventional TSPs based on Ru(terpy)_2Cl_2 as the temperature-sensitive luminophore have temperature sensitivities of less than 2 %K^-1 at 130 K. This sensitivity is not sufficient enough for TSP measurements in large industrial wind tunnels without considerable post-processing effort. The newly developed TSPs achieved a temperature sensitivity of about 4 %K^-1 at 130 K. Experiments were conducted in the cryogenic low-speed wind tunnel of the German-Dutch Wind Tunnel organization to evaluate the capability of these TSPs to detect boundary-layer transition. The new TSP formulations were proven to be capable to resolve small temperature differences and thereby detect boundary-layer transition with high accuracy.

Item URL in elib:https://elib.dlr.de/96571/
Document Type:Conference or Workshop Item (Speech)
Title:Development of a Highly Sensitive Temperature-Sensitive Paint for Measurements under Cryogenic Temperatures (100 – 160 K) Conditions
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Klein, ChristianUNSPECIFIEDhttps://orcid.org/0000-0001-7592-6922UNSPECIFIED
Henne, UlrichUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Costantini, MarcoUNSPECIFIEDhttps://orcid.org/0000-0003-0642-0199134173722
Ondrus, VladimirUni HohenheimUNSPECIFIEDUNSPECIFIED
Beifuss, UweUni HohenheimUNSPECIFIEDUNSPECIFIED
Date:2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI:10.2514/6.2016-0650
Page Range:pp. 1-9
Series Name:Conference Proceedings online
Status:Published
Keywords:TSP (Temperature-Sensitive Paint), cryoTSP, Cryogenic wind tunnel
Event Title:AIAA SciTech 2016 - 54th AIAA Aerospace Sciences Meeting
Event Location:San Diego, CA, USA
Event Type:international Conference
Event Start Date:4 January 2016
Event End Date:8 January 2016
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 - Simulation and Validation (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Micknaus, Ilka
Deposited On:12 May 2016 15:47
Last Modified:24 Apr 2024 20:02

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