User:Paul Lockheed/Sandbox
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where
is indicated airspeed in knots is ISA sea-level speed of sound (661.48 knots) is ISA sea-level pressure (101 325 pascals) is dynamic pressure is ratio of specific heats (1.4)
where
is mach number is static pressure is dynamic pressure
At levels below that where :
At levels above that where :
where
is max operating IAS is ISA sea-level speed of sound (661.48 knots) is static pressure is ISA sea-level pressure is max allowable EAS in knots is max operating mach number is ratio of specific heats (1.4)
where
is element temperature in °celsius is element resistance at t°celsius is resistance at 0°celsius (usually 500 ohms) is 0.003832 is 1.81 is 0 for positive t; 0.1 for negative t
- SAT = TAT / (1 + 0.2 M²) – where M is mach number, and SAT and TAT are in kelvins
- speed of sound (a) = 38.968 √SAT where the SAT is in kelvins (t°celsius + 273.15).
True airspeed is equal to mach number (M) multiplied by the speed of sound (a).