Thomas R Turner
Abstract
From Introduction: The results of the load tests and some additional aerodynamic characteristics of perforated double split flaps on a rectangular NACA 23012 airfoil are given in the present report.
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From Introduction: The results of the load tests and some additional aerodynamic characteristics of perforated double split flaps on a rectangular NACA 23012 airfoil are given in the present report.
Key concepts: Airfoil, NACA airfoil, Aerodynamics, Structural engineering, Engineering, Mechanics, Aerospace engineering, Reynolds number