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AtmosphericModel/scripts/USSA 1976/create_USSA_tables.py
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Python

#!/usr/bin/env python
""" Tables.py - Make tables of atmospheric properties (Python 3)
Adapted by
Richard J. Kwan, Lightsaber Computing
from original programs by
Ralph L. Carmichael, Public Domain Aeronautical Software
Revision History
Date Vers Person Statement of Changes
2004 Oct 04 1.0 RJK Initial program
2017 Jun 04 1.1 RLC All indents are with spaces; all prints in ( )
New version for Python 3 that does integer div with //
"""
import sys, math
version = "1.1 (2017 Jun 04)"
greeting = "Tables - A Python program to compute atmosphere tables"
author = "Ralph L. Carmichael, Public Domain Aeronautical Software"
modifier = "Richard J. Kwan, Lightsaber Computing"
farewell = "Four files added to your directory."
finalmess = "Normal termination of tables."
# P H Y S I C A L C O N S T A N T S
FT2METERS = 0.3048 # mult. ft. to get meters (exact)
KELVIN2RANKINE = 1.8 # mult deg K to get deg R
PSF2NSM = 47.880258 # mult lb/sq.ft to get sq.m
SCF2KCM = 515.379 # mult slugs/cu.ft to get kg/cu.m
TZERO = 288.15 # sea-level temperature, kelvins
PZERO = 101325.0 # sea-level pressure, N/sq.m
RHOZERO = 1.225 # sea-level density, kg/cu.m
AZERO = 340.294 # speed of sound at S.L. m/sec
BETAVISC = 1.458E-6 # viscosity constant
SUTH = 110.4 # Sutherland's constant, kelvins
def LongUSTable():
Itxt = open('us1py.prt', 'w')
Itxt.write(' alt sigma delta theta ')
Itxt.write(' temp press dens a visc k.visc\n')
Itxt.write(' Kft ')
Itxt.write(' degR lb/sq.ft s/cu.ft fps s/ft-s sq.ft/s\n')
for i in range(-1, 57):
altKm=5*i*FT2METERS
(sigma, delta, theta) = Atmosphere(altKm)
Itxt.write("%4i %9.3E %9.3E %6.4f " %
(5*i, sigma, delta, theta))
temp=(KELVIN2RANKINE*TZERO)*theta
pressure=(PZERO/PSF2NSM)*delta
density=(RHOZERO/SCF2KCM)*sigma
asound=(AZERO/FT2METERS)*math.sqrt(theta)
Itxt.write("%5.1f %8.3E %9.3E %6.1f" %
(temp, pressure, density, asound))
viscosity=(1.0/PSF2NSM)*MetricViscosity(theta)
kinematicViscosity=viscosity/density
Itxt.write("%6.3f %8.2E\n" %
(1.0E6*viscosity, kinematicViscosity))
Itxt.close()
def ShortUSTable():
Itxt = open('us2py.prt', 'w')
Itxt.write(' alt sigma delta theta ')
Itxt.write(' temp press dens a visc k.visc ratio\n')
Itxt.write(' Kft ')
Itxt.write(' degR psf s/cu.ft fps s/ft-sec sq.ft/s 1/ft\n')
for i in range(-1, 66):
altKm=i*FT2METERS
(sigma, delta, theta) = SimpleAtmosphere(altKm)
Itxt.write("%4i %6.4f %6.4f %6.4f" %
(i, sigma, delta, theta))
temp=KELVIN2RANKINE*TZERO*theta
pressure=PZERO*delta/47.88
density=RHOZERO*sigma/515.379
asound=(AZERO/FT2METERS)*math.sqrt(theta);
Itxt.write("%6.1f %6.1f %9.7f %6.1f" %
(temp, pressure, density, asound))
viscosity=(1.0/PSF2NSM)*MetricViscosity(theta)
kinematicViscosity=viscosity/density
vratio=asound/kinematicViscosity
Itxt.write("%6.3f %8.2E %4.2f\n"%
(1.0E6*viscosity, kinematicViscosity, 1.0E-6*vratio))
Itxt.close()
def LongSITable():
Itxt = open('si1py.prt', 'w')
Itxt.write(' alt sigma delta theta ')
Itxt.write(' temp press dens a visc k.visc\n')
Itxt.write(' Km ')
Itxt.write(' K N/sq.m kg/cu.m m/sec kg/m-s sq.m/s\n')
for i in range(-4,173):
altKm=0.5*i
(sigma, delta, theta) = Atmosphere(altKm)
Itxt.write("%4.1f %8.4E %8.4E %6.4f" %
(0.5*i, sigma,delta,theta))
temp=TZERO*theta
pressure=PZERO*delta
density=RHOZERO*sigma
asound=AZERO*math.sqrt(theta)
Itxt.write("%6.1f %8.5E %8.3E %5.1f" %
(temp,pressure,density,asound))
viscosity=MetricViscosity(theta)
kinematicViscosity=viscosity/density
Itxt.write("%6.2f %8.2E\n" %
(1.0E6*viscosity, kinematicViscosity))
Itxt.close()
def ShortSITable():
Itxt = open('si2py.prt', 'w')
Itxt.write(' alt sigma delta theta ')
Itxt.write(' temp press dens a visc k.visc ratio\n')
Itxt.write(' Km ')
Itxt.write(' K N/sq.m kcm m/sec kg/m-s sq.m/s 1/m\n')
for i in range(-1, 41):
altKm=0.5*i
(sigma, delta, theta) = SimpleAtmosphere(altKm)
Itxt.write("%4.1f %6.4f %6.4f %6.4f" %
(altKm, sigma, delta, theta))
temp=TZERO*theta
pressure=PZERO*delta
density=RHOZERO*sigma
asound=AZERO*math.sqrt(theta)
Itxt.write("%6.1f %6.0f %5.3f %5.1f" %
(temp, pressure,density,asound))
viscosity=MetricViscosity(theta)
kinematicViscosity=viscosity/density
vratio=asound/kinematicViscosity
Itxt.write("%6.2f %8.2E %5.2f\n" %
(1.0E6*viscosity, kinematicViscosity, 1.0E-6*vratio))
Itxt.close()
def Atmosphere(alt):
""" Compute temperature, density, and pressure in standard atmosphere.
Correct to 86 km. Only approximate thereafter.
Input:
alt geometric altitude, km.
Return: (sigma, delta, theta)
sigma density/sea-level standard density
delta pressure/sea-level standard pressure
theta temperature/sea-level std. temperature
"""
REARTH = 6369.0 # radius of the Earth (km)
GMR = 34.163195
NTAB = 8 # length of tables
htab = [ 0.0, 11.0, 20.0, 32.0, 47.0,
51.0, 71.0, 84.852 ]
ttab = [ 288.15, 216.65, 216.65, 228.65, 270.65,
270.65, 214.65, 186.946 ]
ptab = [ 1.0, 2.2336110E-1, 5.4032950E-2, 8.5666784E-3, 1.0945601E-3,
6.6063531E-4, 3.9046834E-5, 3.68501E-6 ]
gtab = [ -6.5, 0.0, 1.0, 2.8, 0, -2.8, -2.0, 0.0 ]
h = alt*REARTH/(alt+REARTH) # geometric to geopotential altitude
i=0; j=len(htab)-1
while (j > i+1):
k = (i+j)//2 # this is floor division in Python 3
if h < htab[k]:
j = k
else:
i = k
tgrad = gtab[i] # temp. gradient of local layer
tbase = ttab[i] # base temp. of local layer
deltah=h-htab[i] # height above local base
tlocal=tbase+tgrad*deltah # local temperature
theta = tlocal/ttab[0] # temperature ratio
if 0.0 == tgrad:
delta=ptab[i]*math.exp(-GMR*deltah/tbase)
else:
delta=ptab[i]*math.pow(tbase/tlocal, GMR/tgrad)
sigma = delta/theta
return ( sigma, delta, theta )
def SimpleAtmosphere(alt):
""" Compute temperature, density, and pressure in simplified
standard atmosphere.
Correct to 20 km. Only approximate thereafter.
Input:
alt geometric altitude, km.
Return: (sigma, delta, theta)
sigma density/sea-level standard density
delta pressure/sea-level standard pressure
theta temperature/sea-level std. temperature
"""
REARTH = 6369.0 # radius of the Earth (km)
GMR = 34.163195 # gas constant
h = alt*REARTH/(alt+REARTH) # geometric to geopotential altitude
if h<11.0: # troposphere
theta=(288.15-6.5*h)/288.15
delta=math.pow(theta, GMR/6.5)
else: # stratosphere
theta=216.65/288.15
delta=0.2233611*math.exp(-GMR*(h-11.0)/216.65)
sigma = delta/theta
return ( sigma, delta, theta )
def MetricViscosity(theta):
t=theta*TZERO
return BETAVISC*math.sqrt(t*t*t)/(t+SUTH)
def main():
print ("Executing ", sys.argv[0])
print (greeting)
print (author)
if modifier != "":
print ("Modified by ", modifier)
print (" version ", version)
LongUSTable()
ShortUSTable()
LongSITable()
ShortSITable()
print (farewell)
print (finalmess)
main()