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WOLFRAM SYSTEM MODELER

Atmospheres

Atmosphere models

Package Contents

	AtmosphericProperties Property parameters for the U.S. Standard Atmosphere
	atmosphericData Calculates the atmospheric properties at given geometric altitude
	dynamicPressure Calculates dynamic pressure from geometric altitude and velocity
	getHeight Returns geometric altitude from position
	getMach Calculates Mach number
	gravity Function to calculate gravitational acceleration at given geometric altitude

Information

This package contains the functions and data to solve for the atmospheric properties, gravity and Mach number as a function of altitude and total velocity.

Wolfram Language

In[1]:=

SystemModel["Aircraft.Atmospheres"]

Out[1]:=