DocumentCode :
1689792
Title :
Pressure sensitive paint for oscillating pressure fields measurements
Author :
Fonov, S.D. ; Engler, R.H. ; Klein, Cristian
Author_Institution :
Inst. fur Stromungsmech., German Aerosp. Res. Center, Gottingen
fYear :
1999
fDate :
6/21/1905 12:00:00 AM
Abstract :
The paper describes the main problems encountered during investigations of the oscillating pressure fields by the Fast Binary Pressure Sensitive Paint (FBPSP). This formulation has response time in the millisecond range and provides compensation of the model displacements and excitation light instability. Measurement methodology, and theoretical and experimental estimations of the FBPSP dynamic characteristics are presented. It is shown that FBPSP formulation can be used for oscillation frequencies up to 20-40 Hz but requires dynamic compensation of the resulting pressure fields. The experimental results obtained on the pitching wing model at Mach numbers 0.3 and oscillation frequencies 0 and 20 Hz are presented and discussed
Keywords :
flow visualisation; fluorescence; optical sensors; pressure measurement; pressure sensors; radiation quenching; wind tunnels; compensation; dynamic characteristics; excitation light instability; fast binary pressure sensitive paint; luminescence pressure sensors; model displacements; oscillating pressure fields measurement; oxygen quenching; pitching wing model; time response; unsteady flow; Calibration; Delay; Estimation theory; Frequency; Optical sensors; Paints; Polymers; Pressure measurement; Sensor arrays; Temperature sensors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 1999. ICIASF 99. 18th International Congress on
Conference_Location :
Toulouse
Print_ISBN :
0-7803-5715-9
Type :
conf
DOI :
10.1109/ICIASF.1999.827164
Filename :
827164
Link To Document :
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