An investigation of the effects of the sudden extension of a dive-recovery flap on the aerodynamic characteristics of a symmetrical airfoil in two dimensional flow
This report presents the results of an investigation of the aerodynamic characteristics of the NACA symmetrical laminar flow 65,1-012 airfoil. The model was tested with and without a dive recovery flap. The effects obtained by suddenly extending the flap are compared to those obtained with the flap...
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