Bernoulli's Theorem
Bernoulli's theorem states that in a steady, incompressible fluid flow, an increase in fluid velocity results in a decrease in static pressure. In aviation, this explains how air accelerating over the curved upper surface of an aerofoil creates a region of lower static pressure above the wing compared to the lower surface, contributing to lift. Bernoulli's principle works in conjunction with Newton's Third Law — the reaction force from air deflected downward — to fully explain total lift production.
Key Points
- •Relates to the variation of kinetic energy (dynamic pressure) and potential energy (static pressure) within a moving fluid.
- •High-velocity airflow above a wing results in <strong>low static pressure</strong> on the upper surface.
- •Works in conjunction with Coanda theory to explain total lift production.
Exam Relevance
Forms the foundational theoretical knowledge required to understand how wings produce lift and is a frequent multiple-choice question topic.
Related Terms
Learn More
Dive deeper into aerodynamics with our comprehensive study guide.
Aerodynamics Study Guide →Practice Aerodynamics Questions
Test your understanding with exam-style questions. Aerodynamics questions are free — no account needed.