DANIELJ2898 DANIELJ2898

28-09-2022
Physics

Answered

Consider an infinite wing with a naca 1412 airfoil section and a chord length of 3m. The wind is at an angle of attack of 5 degrees in an airflow velocity of 40 m/s at standard sea-level conditions. Calculate the lift, drag, and moment about the quarter-chord per unit span.

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