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    Experimental Determination of the Impact of Floats on the Aerodynamic Characteristics of an OSA Model in Symmetric Flow by Michał FRANT, Stanisław WRZESIEŃ, Maciej MAJCHER

    Published 2021-03-01
    “…The studies have been performed in the low-speed wind tunnel at the Military University of Technology (MUT, Warsaw, Poland). The aircraft model was examined at the dynamic pressure q = 500 Pa in the following angle of attack range alfa= -28 to+28 deg. …”
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