WOLFRAM SYSTEM MODELER
dynamicPressureCalculates dynamic pressure from geometric altitude and velocity |
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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)
Outputs (1)
| q |
Type: Pressure (Pa) Description: Dynamic pressure |
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