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Appropriate Selection of Pressure-Sensitive Paint for Cryogenic Wind Tunnels

Egami, Yasuhiro and Fey, Uwe and Engler, Rolf (2006) Appropriate Selection of Pressure-Sensitive Paint for Cryogenic Wind Tunnels. 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada (USA), 2006-01-09 - 2006-01-12.

Full text not available from this repository.

Abstract

The appropriate combination of a luminophore and a binder for Pressure-Sensitive Paint (PSP) for a cryogenic wind tunnel has been investigated. The sensitivity of a PSP is governed by the luminescence lifetime of a luminophore, the oxygen permeability of a binder and the oxygen partial pressure in a test gas. Test conditions in cryogenic wind tunnels (oxygen concentrations: 0.1% or less, temperatures: 100 – 180 K) are greatly different from those in “warm” wind tunnels (oxygen concentrations: 21%, temperatures: 300-330 K). Therefore, PSPs for a cryogenic wind tunnel demand severe requirements for a luminophore and a binder. In this paper, we studied the necessary conditions of PSP for cryogenic wind tunnels and evaluated them experimentally.

Document Type:Conference or Workshop Item (Speech, Paper)
Additional Information: LIDO-Berichtsjahr=2006, 5 Disc, CD-Code: 778-241002 Vortrag: 26 Folien
Title:Appropriate Selection of Pressure-Sensitive Paint for Cryogenic Wind Tunnels
Authors:
AuthorsInstitution or Email of Authors
Egami, YasuhiroUNSPECIFIED
Fey, UweUNSPECIFIED
Engler, RolfUNSPECIFIED
Date:2006
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Disc 1
Page Range:pp. 1-11
Series Name:AIAA Meeting Papers on Disc
Status:Published
Keywords:cryogenic wind tunnel, Pressure-Sensitive Paint (PSP)
Event Title:44th AIAA Aerospace Sciences Meeting and Exhibit
Event Location:2006-01-09 - 2006-01-12
Event Type:international Conference
Event Dates:Reno, Nevada (USA)
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Experimental Methods
Deposited By: Ilka Micknaus
Deposited On:19 Jun 2006
Last Modified:27 Apr 2009 04:56

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