Flow visualization over a thick blunt trailing-edge airfoil with base cavity at low Reynolds numbers using PIV technique
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چکیده
منابع مشابه
Flow visualization over a thick blunt trailing-edge airfoil with base cavity at low Reynolds numbers using PIV technique
ABSTRACT In this study, the effect of cutting the end of a thick airfoil and adding a cavity on its flow pattern is studied experimentally using PIV technique. First, by cutting 30% chord length of the Riso airfoil, a thick blunt trialing-edge airfoil is generated. The velocity field around the original airfoil and the new airfoil is measured by PIV technique and compared with each other. Then,...
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ژورنال
عنوان ژورنال: Journal of Visualization
سال: 2016
ISSN: 1343-8875,1875-8975
DOI: 10.1007/s12650-016-0405-3