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Flat Earth Debate / Re: "How does a plane follow the curvature of the Earth's atmosphere?"
« on: January 16, 2017, 04:18:38 PM »
Most airliners have two sets of ailerons used for roll control; an inner set which can also be used as a a flap, called a flaperon, and an outer set of ailerons. The outer set gets locked out as the aircrafts speed increases and becomes effective again as the aircraft slows down. This is because at high speed, control surfaces become more effective and less effective at low speeds, therefore only one set is required at cruising speed and both sets provide positive roll control on takeoff and landing. You can see the inner one moving in flight during turbulence and for minor course corrections like avoiding thunderstorms and changing track.
As far as following the curvature of the Earth goes... they dont. Airliners set a standard altimeter setting once passing above what is called the "Transition Altitude". This is 29.92mb in the US or 1013.25 hpa everywhere else in the world. If the cruising altitude is 35,000 feet, the aircraft is flying at the pressure level of 35000 feet, and rarely is it actually 35000 feet above Mean Sea Level.
The autopilot receives an altimeter input and simply maintains the desired pressure altitude. This works because pressure levels in the upper atmosphere are very stratified.
The actual height above ground is called the "Geometric Altitude" and can vary by several thousand feet from the set pressure altitude. This doesn't effect aircraft performance however as all performance predictions for any airliner are based on flying at a standard pressure level rather than a geometric one.
Pressure altitudes are generally higher than the equivalent geometric altitude in the tropics and less than the equivalent in cold climates. It is not unusual in the tropics to be flying at a geometric altitude higher than the maximum altitude for the aircraft whilst flying at a pressure level lower than the maximum.
Hope this helps.
BTW the FE is completely wrong. I'd be dead if it was true.
As far as following the curvature of the Earth goes... they dont. Airliners set a standard altimeter setting once passing above what is called the "Transition Altitude". This is 29.92mb in the US or 1013.25 hpa everywhere else in the world. If the cruising altitude is 35,000 feet, the aircraft is flying at the pressure level of 35000 feet, and rarely is it actually 35000 feet above Mean Sea Level.
The autopilot receives an altimeter input and simply maintains the desired pressure altitude. This works because pressure levels in the upper atmosphere are very stratified.
The actual height above ground is called the "Geometric Altitude" and can vary by several thousand feet from the set pressure altitude. This doesn't effect aircraft performance however as all performance predictions for any airliner are based on flying at a standard pressure level rather than a geometric one.
Pressure altitudes are generally higher than the equivalent geometric altitude in the tropics and less than the equivalent in cold climates. It is not unusual in the tropics to be flying at a geometric altitude higher than the maximum altitude for the aircraft whilst flying at a pressure level lower than the maximum.
Hope this helps.
BTW the FE is completely wrong. I'd be dead if it was true.