Abstract
This chapter presents an overview of existing Gurney flap actuation concepts for rotorcraft applications as well as suggests a new concept applicable to airfoils with little space in the vicinity of airfoil toe. Kinematic and dynamic analysis of the mechanism is performed for the required flap motion pattern. A method of calculating maximum normal force acting on Gurney flap is proposed based on inverse dynamics approach. Piezoelectric actuator force-displacement characteristic and mass properties of mechanism parts are also accounted for in the calculations. A working mock-up of the blade section with active Gurney for wind tunnel testing is designed.
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Berezin, I., Raczynski, R. (2017). Active Gurney Flap Unit. In: Doerffer, P., Barakos, G., Luczak, M. (eds) Recent Progress in Flow Control for Practical Flows. Springer, Cham. https://doi.org/10.1007/978-3-319-50568-8_6
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DOI: https://doi.org/10.1007/978-3-319-50568-8_6
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Publisher Name: Springer, Cham
Print ISBN: 978-3-319-50567-1
Online ISBN: 978-3-319-50568-8
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