What happens aerodynamically as speed approaches the critical Mach number?

Study for the United Airlines Flight Simulator Technician Trade Test. Prepare with flashcards and multiple-choice questions, each with hints and explanations. Get ready for your exam!

Multiple Choice

What happens aerodynamically as speed approaches the critical Mach number?

Explanation:
As speed approaches the critical Mach number, compressibility effects become dominant and the flow over the wing begins to reach supersonic speeds locally while still subsonic overall. This creates a shock wave on the wing surface, usually on the upper cambered part. The shock causes a sharp rise in pressure and a sudden increase in wave drag. It also tends to disrupt the boundary layer, leading to flow separation that reduces lift and can degrade control effectiveness. This combination—a rapid drag rise due to the shock and potential loss of lift or control authority from the altered pressure distribution—matches what happens in this speed regime. The other ideas don’t describe this aerodynamic shift: stall is tied to high angle of attack, engine throttling isn’t an automatic physics effect of Mach numbers, and lift typically doesn’t fall to zero solely because you’re near the critical Mach number.

As speed approaches the critical Mach number, compressibility effects become dominant and the flow over the wing begins to reach supersonic speeds locally while still subsonic overall. This creates a shock wave on the wing surface, usually on the upper cambered part. The shock causes a sharp rise in pressure and a sudden increase in wave drag. It also tends to disrupt the boundary layer, leading to flow separation that reduces lift and can degrade control effectiveness. This combination—a rapid drag rise due to the shock and potential loss of lift or control authority from the altered pressure distribution—matches what happens in this speed regime. The other ideas don’t describe this aerodynamic shift: stall is tied to high angle of attack, engine throttling isn’t an automatic physics effect of Mach numbers, and lift typically doesn’t fall to zero solely because you’re near the critical Mach number.

Subscribe

Get the latest from Examzify

You can unsubscribe at any time. Read our privacy policy