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.
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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/ | ||||||||||||||||||||||||
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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: |
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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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