Theory of Flight Project : Basic Physics

To introduce aviation/aeronautics/aerospace students to wind tunnel(s) and methods used in experimental identification of various aerodynamic (and stability) coefficients of airfoils (2D), wings (3D) and scale models. To understand the value and purpose of wind-tunnel and experimental identification (measurement) of lift, drag, sideforce, and aerodynamic moments (pitching, rolling, yawing). To review the basic aerodynamic theory

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Reference no: EM132069492

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