DocumentCode :
2773104
Title :
Use of pressure-sensitive paints in low-speed flows
Author :
Morris, Martin J.
Author_Institution :
McDonnell Douglas Corp., St. Louis, MO, USA
fYear :
1995
fDate :
18-21 Jul 1995
Lastpage :
3110
Abstract :
Pressure measurements based on pressure-sensitive paint (PSP) have been shown to be useful in low speed flows. Many obstacles were addressed in making these successful measurements. The considerations for making these measurements are presented, as well as, a brief discussion of important procedures. A sample of data is presented to demonstrate the agreement between pressure-sensitive paint and traditional pressure taps
Keywords :
aircraft testing; photoluminescence; pressure measurement; wind tunnels; low-speed flows; photoluminescent coatings; pressure measurements; pressure-sensitive paints; wind tunnel testing; Coatings; Hardware; Luminescence; Measurement errors; Paints; Pressure measurement; Signal resolution; Testing; Velocity measurement; Wind speed;
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.1995.519137
Filename :
519137
Link To Document :
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