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Application of Lifetime-based Pressure-Sensitive Paint Technique to Cryogenic Wind Tunnel Tests

Yorita, Daisuke and Klein, Christian and Henne, Ulrich and Ondrus, Vladimir and Beifuss, Uwe and Hensch, Ann-Katrin and Guntermann, Peter and Quest, Jürgen (2016) Application of Lifetime-based Pressure-Sensitive Paint Technique to Cryogenic Wind Tunnel Tests. AIAA SciTech 2016 - 54th AIAA Aerospace Sciences Meeting, 04. - 08. Jan. 2016, San Diego, CA, USA. DOI: 10.2514/6.2016-0649

Full text not available from this repository.

Official URL: http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0649

Abstract

The capability of a lifetime-based Pressure-Sensitive Paint (PSP) method for application in cryogenic wind tunnels was investigated. The relevant experiments were conducted in the Pilot-European Transonic Windtunnel (PETW). The 2D airfoil model (CAST10-II) was painted with PtTFPP/PTMSP paint and tested in a nitrogen atmosphere at 150 K. PSP and pressure tap data were acquired at Mach 0.78 at a total pressure of 160 kPa. The oxygen concentration of the flow was set to 1000 ppm by continuously supplying dry air. As a result, the lifetime-based PSP method successfully visualized the pressure distribution on the airfoil model under cryogenic conditions. The quantitative agreement of PSP and pressure tap data was obtained and the difference in both data came out to be 0.05 in the pressure coefficient Cp. The accuracy of PSP data is comparable to results achievable at ambient conditions. Therefore, it may be concluded that the lifetime-based method was successfully applied under cryogenic conditions. In addition to the lifetime-based method, the intensity-based method was also conducted as a comparison. Furthermore the applicability of the lifetimebased method to tests with model deformation was evaluated.

Item URL in elib:https://elib.dlr.de/96572/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA 2016-0649
Title:Application of Lifetime-based Pressure-Sensitive Paint Technique to Cryogenic Wind Tunnel Tests
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Yorita, Daisukedaisuke.yorita (at) dlr.deUNSPECIFIED
Klein, ChristianChristian.Klein (at) dlr.deUNSPECIFIED
Henne, Ulrichulrich.henne (at) dlr.deUNSPECIFIED
Ondrus, VladimirUni HohenheimUNSPECIFIED
Beifuss, UweUni HohenheimUNSPECIFIED
Hensch, Ann-KatrinEuropean Transonic Windtunnel (ETW), 51147 Cologne, GermanyUNSPECIFIED
Guntermann, PeterEuropean Transonic Windtunnel (ETW), 51147 Cologne, GermanyUNSPECIFIED
Quest, JürgenETWUNSPECIFIED
Date:2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2016-0649
Page Range:pp. 1-10
Series Name:Conference Proceedings online
Status:Published
Keywords:PSP (Pressure-Sensitive Paint), Cryogenic wind tunnel, Lifetime-based Method
Event Title:AIAA SciTech 2016 - 54th AIAA Aerospace Sciences Meeting
Event Location:San Diego, CA, USA
Event Type:international Conference
Event Dates:04. - 08. Jan. 2016
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
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Micknaus, Ilka
Deposited On:18 May 2016 09:59
Last Modified:18 May 2016 09:59

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