WOLFRAM SYSTEM MODELER

getMach

Calculates Mach number

Wolfram Language

In[1]:=
SystemModel["Aircraft.Atmospheres.getMach"]
Out[1]:=

Information

Calculates Mach number for given total velocity and geometric altitude.

Syntax

mach = getMach(h, v)

Inputs (2)

h

Type: Height (m)

Description: Geometrical altitude

v

Type: Velocity (m/s)

Description: Velocity (true airspeed)

Outputs (1)

mach

Type: MachNumber

Description: Mach number