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You will study the structure of aerofoils, including critical components such as the chord line, camber, and leading-edge radius, and how their design influences flight performance. You will explore Bernoulli’s Principle and its role in creating pressure differentials, examine how airflow distribution impacts lift and drag, and apply the lift equation to real-world flying scenarios. Through this knowledge, you will be equipped to make informed decisions as a pilot, particularly regarding flap deployment, angle of attack adjustments, and airspeed control to achieve optimal lift.
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This course includes 2 modules, 5 lessons, and 2:00 hours of materials.
This course explores the essential aerofoil terminology, Bernoulli’s Principle, pressure distribution, and the lift equation, giving learners an in-depth understanding of how lift is produced, controlled, and optimized in various flight conditions.
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