DocumentCode :
2942243
Title :
Application of piezoelectric foils in experimental aerodynamics
Author :
Nitsche, W. ; Mirow, P. ; Dörfler, T.
Author_Institution :
Inst. fur Luft- und Raumfahrt, Tech. Univ. Berlin, West Germany
fYear :
1989
fDate :
18-21 Sep 1989
Firstpage :
57
Lastpage :
65
Abstract :
The authors outline basic aspects of the use of piezo foils and multisensor piezo arrays in flow experiments. They survey some piezo foil applications in the field of experimental aerodynamics, including wind tunnel and free flight tests of airfoils, and they conduct a more general investigation of unsteady surface forces on flow around bodies. It is concluded that the piezo foil technique is useful for flow experiments aiming at characterizing airfoil flows by means of sensing unsteady surface forces. Preliminary results of the application of array, raster, and matrix sensors for monitoring flow instabilities are very encouraging
Keywords :
aerodynamics; electric sensing devices; flow instability; flow measurement; piezoelectric transducers; wind tunnels; airfoil flows; airfoils; array sensor; experimental aerodynamics; flow experiments; flow instabilities; free flight tests; matrix sensors; multisensor piezo arrays; piezo foil; piezoelectric foils; raster sensor; unsteady surface forces; wind tunnel; Aerodynamics; Coatings; Force measurement; Metallization; Piezoelectric transducers; Polymer films; Sensor arrays; Sensor systems; Standards development; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 1989. ICIASF '89 Record., International Congress on
Conference_Location :
Gottingen
Type :
conf
DOI :
10.1109/ICIASF.1989.77659
Filename :
77659
Link To Document :
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