DocumentCode :
2929331
Title :
Application of PSP To the Study of 3D Shock-Boundary Layer Interaction
Author :
Raju, Channa ; Viswanath, P.R
Author_Institution :
Experimental Aerodynamics Division, National Aerospace Laboratories, Bangalore-560 017, INDIA. Email: craju@ead.cmmacs.ernet.in
fYear :
2005
fDate :
2005
Firstpage :
197
Lastpage :
201
Abstract :
Experiments have been performed documenting the pressure field using a PSP technique in blunt fin-induced turbulent boundary layer interactions at a freestream Mach number of 1.8. Three blunt fins of different nose diameters have been tested in this study. The PSP measurements were made using the well known Optrod-B1 binary pressure sensitive paint. Excellent agreement of PSP results with conventional static pressure measurements has been observed.
Keywords :
Aerodynamics; Aerospace testing; Laboratories; Nose; Paints; Plugs; Pressure measurement; Prototypes; Tail; Visualization;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 2005. iciasf '05. 21st International Congress on
Print_ISBN :
0-7803-9096-2
Type :
conf
DOI :
10.1109/ICIASF.2005.1569923
Filename :
1569923
Link To Document :
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