As the airflow over the upper surface increases, static pressure and dynamic pressure change how?

Prepare for the Theory of Rotary Wing Flight Test. Sharpen your skills with flashcards and multiple choice questions, with hints and explanations for each. Ace your exam with confidence!

Multiple Choice

As the airflow over the upper surface increases, static pressure and dynamic pressure change how?

Explanation:
As the local airflow over the upper surface speeds up, the air there has more kinetic energy, so the dynamic pressure increases. Bernoulli’s principle for steady, incompressible flow says the sum of static and dynamic pressure is roughly constant along a streamline. Since dynamic pressure rises with speed (q = 1/2 ρV²), the static pressure must fall where the velocity increases. So the upper surface experiences a decrease in static pressure while the dynamic pressure increases as the flow accelerates. This contrast—lower static pressure and higher dynamic pressure on the fast-moving upper surface—helps explain why the top surface has lower pressure and contributes to lift.

As the local airflow over the upper surface speeds up, the air there has more kinetic energy, so the dynamic pressure increases. Bernoulli’s principle for steady, incompressible flow says the sum of static and dynamic pressure is roughly constant along a streamline. Since dynamic pressure rises with speed (q = 1/2 ρV²), the static pressure must fall where the velocity increases. So the upper surface experiences a decrease in static pressure while the dynamic pressure increases as the flow accelerates. This contrast—lower static pressure and higher dynamic pressure on the fast-moving upper surface—helps explain why the top surface has lower pressure and contributes to lift.

Subscribe

Get the latest from Examzify

You can unsubscribe at any time. Read our privacy policy