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It works by reading the difference between static pressure and total pressure from air flowing into a pitottube. For instance, an aircraft maintaining a steady IAS at 30,000 feet will have a faster TAS than at sea level due to reduced drag from thinner air. This means less drag and faster ground speed.
And ice doesn’t just make things slippery, it messes with the airflow over the wings, cuts down on lift, and ramps up drag. This leads to a serious loss of lift and an increase in drag. This roughness adds to friction drag, which can reduce lift and increase drag by as much as 50% on a wing’s leading edge and upper surface.
Ram air from a pitottube and static (undisturbed) outside air from a static port, usually a hole on the side of the fuselage. Airspeed indicators need air from a pitottube and static air from a static port Small general aviation aircraft have airspeed indicators with air hoses connected directly to the pitot and static sources.
Foust would describe the incident thusly: “The aircraft looked like the pitottube was stationary with the aircraft rotating around it. Foust did everything in his training to try and recover from the spin, including deploying his plane’s drag chute. Very flat and rotating quite slowly.
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