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    Design and Numerical Calculation of Variable Test Section for Small Supersonic Wind Tunnel by Václav DVOŘÁK, Oldřich STUPKA, Jan KOLÁŘ

    Published 2010-12-01
    “…Computed distributions of Cp along the airfoil are verified by comparison with experimental data, which were obtained by measurements in a closed circuit wind tunnel at the constant Reynolds number and several angles of attack. …”
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