TrueAirspeed | R Documentation |
Returns the true airspeed
TrueAirspeed(MACH, AT, EoverP = 0)
MACH |
A numeric vector representing the Mach number, possibly from MachNumber() |
AT |
A numeric vector representing the air temperature in deg.C |
EoverP |
An optional numeric vector representing the ratio of water vapor pressure to total pressure |
Calculates the true airspeed from measurements of Mach number, air temperature, and optionally humidity
A numeric vector giving the true airspeed in m/s
William Cooper
TAS <- TrueAirspeed (MachNumber (RAFdata$PSXC, RAFdata$QCXC), RAFdata$ATX, RAFdata$EWX/RAFdata$PSXC)
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