This Mechanical Engineering lab report details two experiments in fluid mechanics. The first experiment investigates the pressure distribution around a NACA 0012 aerofoil at varying angles of attack, measuring the coefficient of pressure (Cp) at different tapping points and determining the center of pressure. The results, presented in graphs of Cp against x, show how the angle of attack affects lift and drag. The second experiment explores Bernoulli's theorem using a Venturi meter, aiming to calculate fluid velocity at different points. The report includes methodology, experimental setup, results, calculations, and discussions, providing a comprehensive analysis of fluid flow principles. The report also adheres to the guidelines provided, including safety measures and general instructions for conducting the laboratory experiments.
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