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Showing 1 to 1 of 1 for “"flap-chord ratio"”.

  1. Experimental wind tunnel study of airfoils with large flap deflections at low Reynolds numbers

    … for four airfoils with trailing edge plain flaps in an attempt to understand the effects of Reynolds number, percent thickness (t/c), percent chord of flap (flap-chord ratio), and flap deflection on airfoil performance. The four airfoils used in this research were the AG40d-02r, AG455ct-02r, …

    uiuc Repository record for Experimental wind tunnel study of airfoils with large flap deflections at low Reynolds numbers (opens in a new tab)