DocumentCode
2834554
Title
Pressure sensitive paint application in shock wind tunnel
Author
Borovoy, V. ; Bykov, A. ; Mosharov, V. ; Orlov, A. ; Radchenko, V. ; Phonov, S.
Author_Institution
Central AeroHydrodynamic Inst., Zhukovsky, Russia
fYear
1995
fDate
18-21 Jul 1995
Abstract
Pressure sensitive paint technology is a new optical pressure measurement method providing new opportunities for non-contact pressure measurements. Specific features of PSP-technology for shock wind tunnel are discussed. An optical pressure measurement system for instantaneous measurements is described. Results of pressure measurements on a cylinder at Mach 6 are presented
Keywords
photoluminescence; pressure measurement; wind tunnels; Mach 6; PSP-technology; cylinder; instantaneous measurements; noncontact pressure measurements; optical pressure measurement method; paint technology; photoluminescence; pressure sensitive paint; shock wind tunnel; Aerodynamics; Electric shock; Luminescence; NASA; Optical sensors; Paints; Polymers; Pressure measurement; Temperature; Thickness measurement;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 1995. ICIASF '95 Record., International Congress on
Conference_Location
Wright-Patterson AFB, OH
Print_ISBN
0-7803-2088-3
Type
conf
DOI
10.1109/ICIASF.1995.519465
Filename
519465
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