Aircraft speed: Difference between revisions

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*'''Equivalent''' airspeed (EAS) takes into account another correction (above [[#Calibrated airspeed]], this time having to do with air properties rather than sensor errors.  
*'''Equivalent''' airspeed (EAS) takes into account another correction (above [[#Calibrated airspeed]], this time having to do with air properties rather than sensor errors.  


At high altitude, the compressibility of air changes, so even CAS becomes more and more unreliable. For the SR-71 Blackbird with a ceiling of 85.000 foot, the CAS becomes very unreliable and the plane has to be flown based on a KEAS. For more conventional aircraft, EAS is not used. Thus, EAS is what a perfect dynamic pressure sensor would show when properly calibrated for the air compressibility at the current altitude.
At high altitude, the compressibility of air changes, so even CAS becomes more and more unreliable. For the SR-71 Blackbird with a ceiling of 85.000 feet, the CAS becomes very unreliable and the plane has to be flown based on a KEAS. For more conventional aircraft, EAS is not used. Thus, EAS is what a perfect dynamic pressure sensor would show when properly calibrated for the air compressibility at the current altitude.


=== Mach number ===
=== Mach number ===
1,669

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