WOLFRAM SYSTEM MODELER

dynamicPressure

Calculates dynamic pressure from geometric altitude and velocity

Wolfram Language

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

Information

This function takes the geometric altitude and aircraft total velocity as inputs and returns the dynamic pressure.

Syntax

q = dynamicPressure(h, v)

Inputs (2)

h

Type: Height (m)

Description: Geometrical altitude
v

Type: Velocity (m/s)

Description: Aircraft speed

Outputs (1)

q

Type: Pressure (Pa)

Description: Dynamic pressure