TrueAirspeed: TrueAirspeed
In WilliamCooper/Ranadu: Functions for use with RAF aircraft data files
Description
Usage
Arguments
Details
Value
Author(s)
Examples
Description
Returns the true airspeed
Usage
1
TrueAirspeed(MACH, AT, EoverP = 0)
Arguments
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
Details
Calculates the true airspeed from measurements of Mach number, air temperature, and optionally humidity
Value
A numeric vector giving the true airspeed in m/s
Author(s)
William Cooper
Examples
1
WilliamCooper/Ranadu documentation built on July 10, 2019, 12:40 a.m.
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Description Usage Arguments Details Value Author(s) Examples
Description
Returns the true airspeed
Usage
1 | TrueAirspeed(MACH, AT, EoverP = 0)
|
Arguments
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 |
Details
Calculates the true airspeed from measurements of Mach number, air temperature, and optionally humidity
Value
A numeric vector giving the true airspeed in m/s
Author(s)
William Cooper
Examples
1 |
R Package Documentation
Browse R Packages
We want your feedback!
Note that we can't provide technical support on individual packages. You should contact the package authors for that.
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