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Assessment of PIV-based unsteady load determination of an airfoil with actuated flap
Institution:1. Aerospace Centre of Excellence, University of Strathclyde, 75 Montrose street, Glasgow, United Kingdom;2. Department of Mathematics and Statistics, University of Strathclyde, 26 Richmond street, Glasgow, United Kingdom;2. Delft University of Technology, The Netherlands
Abstract:
Keywords:Unsteady load  PIV  Noca's method  Oscillating flap  Wind tunnel corrections
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