In supersonic airflow, static pressure behind an expansion wave will

Get ready for the AASA Aviation Exam with our comprehensive study tool featuring flashcards and multiple choice questions. Each question provides hints and explanations. Ace your aviation exam with confidence!

Multiple Choice

In supersonic airflow, static pressure behind an expansion wave will

Explanation:
In supersonic flow, turning the flow away from its direction creates a Prandtl–Meyer expansion fan, which is an isentropic expansion. As the flow expands, it accelerates (Mach number increases) and the static pressure drops. This energy shifting from pressure to kinetic energy lowers the static pressure behind the expansion wave compared with the pressure ahead of it. So the static pressure behind the expansion wave decreases relative to the pressure ahead.

In supersonic flow, turning the flow away from its direction creates a Prandtl–Meyer expansion fan, which is an isentropic expansion. As the flow expands, it accelerates (Mach number increases) and the static pressure drops. This energy shifting from pressure to kinetic energy lowers the static pressure behind the expansion wave compared with the pressure ahead of it. So the static pressure behind the expansion wave decreases relative to the pressure ahead.

Subscribe

Get the latest from Passetra

You can unsubscribe at any time. Read our privacy policy