Soar to New Heights: 2026 Commercial Pilot Aerodynamics Adventure Test!

Session length

1 / 20

Which of the following is a potential consequence when accelerating through the critical Mach number?

Increased Cruising Altitude Capability

Decreased Airframe Wear

Control Difficulties

As you push through the critical Mach number, airflow over the wing becomes compressible and shock waves form. These shocks change the pressure distribution, causing lift and drag to shift suddenly. More importantly for handling, the flow can separate around control surfaces, reducing their effectiveness and producing buffet. That combination makes piloting more difficult, with stick forces and response becoming less predictable.

Other options don’t fit because cruising altitude capability is set by engine and airframe design, not simply breaking Mcrit; airframe wear doesn't decrease just from reaching transonic speeds and can even increase from buffet loads; and fuel consumption typically does not drop in this regime—wave drag generally increases, making transonic flight less fuel-efficient.

Reduced Fuel Consumption

Next Question
Subscribe

Get the latest from Examzify

You can unsubscribe at any time. Read our privacy policy