Atmospheric Model¶
The basis of our simulation is a model of Earth’s atmosphere, of which there are several. The International Standard Atmosphere (ISA) is used by ICAO, is relatively simple, and accurate enough for our purposes.
The ISA is a mathematical model of the atmosphere that assumes a linear temperature gradient against altitude, and derives pressure and density from the ideal gas law and hydrostatic equilibrium.
Symbols used¶
Since the primary source upon which the models in this package are built from is the ISA, I will use the symbols defined in the paper that defined it.
from preamble import *
symbol_table
## WIP
Symbol | Description |
---|---|
$A$ | Area |
$C_{d}$ | Coefficient of drag |
$D$ | Diameter |
$F$ | Force |
$F_{d}$ | Force of drag |
$F_{g}$ | Force of gravity |
$g$ | Acceleration due to gravity |
$H$ | Geopotential height |
$h$ | Geometric height |
$P$ | Pressure |
$P_{b}$ | Pressure at the base of an atmospheric layer |
$M$ | Molecular mass |
$m$ | Mass |
$n$ | Amount of substance |
$R^{*}$ | Universal gas constant |
$R$ | Specific gas constant |
$T$ | Thermodynamic temperature |
$V$ | Volume |
$v$ | Velocity |
$\rho$ | Density |