FLAP GAP OSCILLATORY BLOWING ON 2D AND 2.5D WING

Flap Gap Oscillatory Blowing on 2D and 2.5D Wing

Here we present preliminary results obtained in developing an active flow control system for highlift systems at advanced TRL level.The Electronic Speed Controllers work is based on theoretical and experimental workperformed in AVERT EU FP6 project where the oscillatory flap gap blowing system was designedand tested on a INCAS F15 2D wing model.Pre

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Applying for, Operating, and Renewing a Research Experience for Undergraduates Site Program in Computational Biology

We Alarms reflected on our experience in applying for, operating, and renewing a Research Experience for Undergraduates Site program in computational biology from 2016 to 2021 at a metropolitan public university, funded by the National Science Foundation of the U.S.A.Our mistakes during the application process were avoidable in retrospect.Our Inter

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