import numpy as np
CtoK = 273.16 # 273.15
""" Conversion factor for (^\circ\,C) to (^\\circ\\,K) """
kappa = 0.4 # NOTE: 0.41
""" von Karman's constant """
# ---------------------------------------------------------------------
def cdn_calc(u10n, Ta, Tp, lat, meth="S80"):
""" Calculates neutral drag coefficient
Parameters
----------
u10n : float
neutral 10m wind speed (m/s)
Ta : float
air temperature (K)
Tp : float
wave period
meth : str
Returns
-------
cdn : float
"""
if (meth == "S80"):
cdn = np.where(u10n <= 3, (0.61+0.567/u10n)*0.001,
(0.61+0.063*u10n)*0.001)
elif (meth == "LP82"):
cdn = np.where((u10n < 11) & (u10n >= 4), 1.2*0.001,
np.where((u10n <= 25) & (u10n >= 11),
(0.49+0.065*u10n)*0.001, 1.14*0.001))
elif (meth == "S88" or meth == "UA" or meth == "ERA5" or meth == "C30" or
meth == "C35" or meth == "C40"):
cdn = cdn_from_roughness(u10n, Ta, None, lat, meth)
elif (meth == "YT96"):
# for u<3 same as S80
cdn = np.where((u10n < 6) & (u10n >= 3),
(0.29+3.1/u10n+7.7/u10n**2)*0.001,
np.where((u10n <= 26) & (u10n >= 6),
(0.60 + 0.070*u10n)*0.001, (0.61+0.567/u10n)*0.001))
elif (meth == "LY04"):
cdn = np.where(u10n >= 0.5,
(0.142+(2.7/u10n)+(u10n/13.09))*0.001, np.nan)
else:
print("unknown method cdn: "+meth)
return cdn
# ---------------------------------------------------------------------
def cdn_from_roughness(u10n, Ta, Tp, lat, meth="S88"):
""" Calculates neutral drag coefficient from roughness length
Parameters
----------
u10n : float
neutral 10m wind speed (m/s)
Ta : float
air temperature (K)
Tp : float
wave period
meth : str
Returns
-------
cdn : float
"""
g, tol = gc(lat, None), 0.000001
cdn, usr = np.zeros(Ta.shape), np.zeros(Ta.shape)
cdnn = (0.61+0.063*u10n)*0.001
zo, zc, zs = np.zeros(Ta.shape), np.zeros(Ta.shape), np.zeros(Ta.shape)
for it in range(5):
cdn = np.copy(cdnn)
usr = np.sqrt(cdn*u10n**2)
if (meth == "S88"):
# Charnock roughness length (eq. 4 in Smith 88)
zc = 0.011*np.power(usr, 2)/g
# smooth surface roughness length (eq. 6 in Smith 88)
zs = 0.11*visc_air(Ta)/usr
zo = zc + zs # eq. 7 & 8 in Smith 88
elif (meth == "UA"):
# valid for 0<u<18m/s # Zeng et al. 1998 (24)
zo = 0.013*np.power(usr, 2)/g+0.11*visc_air(Ta)/usr
elif (meth == "C30"):
a = 0.011*np.ones(Ta.shape)
a = np.where(u10n > 10, 0.011+(u10n-10)/(18-10)*(0.018-0.011),
np.where(u10n > 18, 0.018, a))
zo = a*np.power(usr, 2)/g+0.11*visc_air(Ta)/usr
elif (meth == "C35"):
a = 0.011*np.ones(Ta.shape)
# a = np.where(u10n > 19, 0.0017*19-0.0050,
# np.where((u10n > 7) & (u10n <= 18),
# 0.0017*u10n-0.0050, a))
a = np.where(u10n > 19, 0.0017*19-0.0050, 0.0017*u10n-0.0050)
zo = 0.11*visc_air(Ta)/usr+a*np.power(usr, 2)/g
elif (meth == "C40"):
a = 0.011*np.ones(Ta.shape)
a = np.where(u10n > 22, 0.0016*22-0.0035, 0.0016*u10n-0.0035)
zo = a*np.power(usr, 2)/g+0.11*visc_air(Ta)/usr # surface roughness
elif (meth == "ERA5"):
# eq. (3.26) p.40 over sea IFS Documentation cy46r1
zo = 0.11*visc_air(Ta)/usr+0.018*np.power(usr, 2)/g
else:
print("unknown method for cdn_from_roughness "+meth)
cdnn = (kappa/np.log(10/zo))**2
cdn = np.where(np.abs(cdnn-cdn) < tol, cdnn, np.nan)
return cdnn
# ---------------------------------------------------------------------
def ctcqn_calc(zol, cdn, u10n, zo, Ta, meth="S80"):
""" Calculates neutral heat and moisture exchange coefficients
Parameters
----------
zol : float
height over MO length
cdn : float
neatral drag coefficient
u10n : float
neutral 10m wind speed (m/s)
zo : float
surface roughness (m)
Ta : float
air temperature (K)
meth : str
Returns
-------
ctn : float
neutral heat exchange coefficient
cqn : float
neutral moisture exchange coefficient
"""
if (meth == "S80" or meth == "S88" or meth == "YT96"):
cqn = np.ones(Ta.shape)*1.20*0.001 # from S88
ctn = np.ones(Ta.shape)*1.00*0.001
elif (meth == "LP82"):
cqn = np.where((zol <= 0) & (u10n > 4) & (u10n < 14), 1.15*0.001,
1*0.001)
ctn = np.where((zol <= 0) & (u10n > 4) & (u10n < 25), 1.13*0.001,
0.66*0.001)
elif (meth == "LY04"):
cqn = 34.6*0.001*np.sqrt(cdn)
ctn = np.where(zol <= 0, 32.7*0.001*np.sqrt(cdn), 18*0.001*np.sqrt(cdn))
elif (meth == "UA"):
usr = np.sqrt(cdn*np.power(u10n, 2))
# Zeng et al. 1998 (25)
re=usr*zo/visc_air(Ta)
zoq = zo/np.exp(2.67*np.power(re, 1/4)-2.57)
zot = zoq
cqn = np.where((u10n > 0.5) & (u10n < 18), np.power(kappa, 2) /
(np.log(10/zo)*np.log(10/zoq)), np.nan)
ctn = np.where((u10n > 0.5) & (u10n < 18), np.power(kappa, 2) /
(np.log(10/zo)*np.log(10/zoq)), np.nan)
elif (meth == "C30"):
usr = np.sqrt(cdn*np.power(u10n, 2))
rr = zo*usr/visc_air(Ta)
zoq = np.where(5e-5/np.power(rr, 0.6) > 1.15e-4, 1.15e-4,
5e-5/np.power(rr, 0.6)) # moisture roughness
zot=zoq # temperature roughness
cqn = kappa**2/np.log(10/zo)/np.log(10/zoq)
ctn = kappa**2/np.log(10/zo)/np.log(10/zot)
elif (meth == "C35"):
usr = np.sqrt(cdn*np.power(u10n, 2))
rr = zo*usr/visc_air(Ta)
zoq = np.where(5.8e-5/np.power(rr, 0.72) > 1.6e-4, 1.6e-4,
5.8e-5/np.power(rr, 0.72)) # moisture roughness
zot=zoq # temperature roughness
cqn = kappa**2/np.log(10/zo)/np.log(10/zoq)
ctn = kappa**2/np.log(10/zo)/np.log(10/zot)
elif (meth == "C40"):
usr = np.sqrt(cdn*np.power(u10n, 2))
rr = zo*usr/visc_air(Ta)
zot = np.where(1.0e-4/np.power(rr, 0.55) > 2.4e-4/np.power(rr, 1.2),
2.4e-4/np.power(rr, 1.2),
1.0e-4/np.power(rr, 0.55)) # temperature roughness
zoq = np.where(2.0e-5/np.power(rr,0.22) > 1.1e-4/np.power(rr,0.9),
1.1e-4/np.power(rr,0.9), 2.0e-5/np.power(rr,0.22))
# moisture roughness determined by the CLIMODE, GASEX and CBLAST data
# zoq = np.where(5e-5/np.power(rr, 0.6) > 1.15e-4, 1.15e-4,
# 5e-5/np.power(rr, 0.6)) # moisture roughness as in C30
cqn = kappa**2/np.log(10/zo)/np.log(10/zoq)
ctn = kappa**2/np.log(10/zo)/np.log(10/zot)
elif (meth == "ERA5"):
# eq. (3.26) p.40 over sea IFS Documentation cy46r1
usr = np.sqrt(cdn*np.power(u10n, 2))
zot = 0.40*visc_air(Ta)/usr
zoq = 0.62*visc_air(Ta)/usr
cqn = kappa**2/np.log(10/zo)/np.log(10/zoq)
ctn = kappa**2/np.log(10/zo)/np.log(10/zot)
else:
print("unknown method ctcqn: "+meth)
return ctn, cqn
# ---------------------------------------------------------------------
def cd_calc(cdn, height, ref_ht, psim):
""" Calculates drag coefficient at reference height
Parameters
----------
cdn : float
neutral drag coefficient
height : float
original sensor height (m)
ref_ht : float
reference height (m)
psim : float
momentum stability function
Returns
-------
cd : float
"""
cd = (cdn*np.power(1+np.sqrt(cdn)*np.power(kappa, -1) *
(np.log(height/ref_ht)-psim), -2))
return cd
# ---------------------------------------------------------------------
def ctcq_calc(cdn, cd, ctn, cqn, h_t, h_q, ref_ht, psit, psiq):
""" Calculates heat and moisture exchange coefficients at reference height
Parameters
----------
cdn : float
neutral drag coefficient
cd : float
drag coefficient at reference height
ctn : float
neutral heat exchange coefficient
cqn : float
neutral moisture exchange coefficient
h_t : float
original temperature sensor height (m)
h_q : float
original moisture sensor height (m)
ref_ht : float
reference height (m)
psit : float
heat stability function
psiq : float
moisture stability function
Returns
-------
ct : float
cq : float
"""
ct = ctn*(cd/cdn)**0.5/(1+ctn*((np.log(h_t/ref_ht)-psit)/(kappa*cdn**0.5)))
cq = cqn*(cd/cdn)**0.5/(1+cqn*((np.log(h_q/ref_ht)-psiq)/(kappa*cdn**0.5)))
return ct, cq
# ---------------------------------------------------------------------
def psim_calc(zol, meth="S80"):
""" Calculates momentum stability function
Parameters
----------
zol : float
height over MO length
meth : str
Returns
-------
psim : float
"""
coeffs = get_stabco(meth)
alpha, beta, gamma = coeffs[0], coeffs[1], coeffs[2]
if (meth == "ERA5"):
psim = np.where(zol < 0, psim_conv(zol, alpha, beta, gamma),
psim_stab_era5(zol, alpha, beta, gamma))
elif (meth == "C30" or meth == "C35" or meth == "C40"):
psim = psiu_26(zol, meth)
else:
psim = np.where(zol < 0, psim_conv(zol, alpha, beta, gamma),
psim_stab(zol, alpha, beta, gamma))
return psim
# ---------------------------------------------------------------------
def psit_calc(zol, meth="S80"):
""" Calculates heat stability function
Parameters
----------
zol : float
height over MO length
meth : str
Returns
-------
psit : float
"""
coeffs = get_stabco(meth)
alpha, beta, gamma = coeffs[0], coeffs[1], coeffs[2]
if (meth == "ERA5"):
psit = np.where(zol < 0, psi_conv(zol, alpha, beta, gamma),
psi_stab_era5(zol, alpha, beta, gamma))
elif (meth == "C30" or meth == "C35" or meth == "C40"):
psit = psit_26(zol)
else:
psit = np.where(zol < 0, psi_conv(zol, alpha, beta, gamma),
psi_stab(zol, alpha, beta, gamma))
return psit
# ---------------------------------------------------------------------
def get_stabco(meth="S80"):
""" Gives the coefficients \\alpha, \\beta, \\gamma for stability functions
Parameters
----------
meth : str
Returns
-------
coeffs : float
"""
if (meth == "S80" or meth == "S88" or meth == "LY04" or
meth == "UA" or meth == "ERA5" or meth == "C30" or meth == "C35" or
meth == "C40"):
alpha, beta, gamma = 16, 0.25, 5 # Smith 1980, from Dyer (1974)
elif (meth == "LP82"):
alpha, beta, gamma = 16, 0.25, 7
elif (meth == "YT96"):
alpha, beta, gamma = 20, 0.25, 5
else:
print("unknown method stabco: "+meth)
coeffs = np.zeros(3)
coeffs[0] = alpha
coeffs[1] = beta
coeffs[2] = gamma
return coeffs
# ---------------------------------------------------------------------
def psi_stab_era5(zol, alpha, beta, gamma):
""" Calculates heat stability function for stable conditions
for method ERA5
Parameters
----------
zol : float
height over MO length
alpha, beta, gamma : float
constants given by get_stabco
Returns
-------
psit : float
"""
# eq (3.22) p. 39 IFS Documentation cy46r1
a, b, c, d = 1, 2/3, 5, 0.35
psit = -b*(zol-c/d)*np.exp(-d*zol)-np.power(1+(2/3)*a*zol, 1.5)-(b*c)/d+1
return psit
# ---------------------------------------------------------------------
def psit_26(zol):
""" Computes temperature structure function as in C35
Parameters
----------
zol : float
height over MO length
Returns
-------
psi : float
"""
b, d = 2/3, 0.35
dzol = np.where(d*zol > 50, 50, d*zol) # stable
psi = -((1+b*zol)**1.5+b*(zol-14.28)*np.exp(-dzol)+8.525)
psik = 2*np.log((1+np.sqrt(1-15*zol))/2)
psic = (1.5*np.log((1+np.power(1-34.15*zol, 1/3) +
np.power(1-34.15*zol, 2/3))/3)-np.sqrt(3) *
np.arctan(1+2*np.power(1-34.15*zol, 1/3))/np.sqrt(3) +
4*np.arctan(1)/np.sqrt(3))
f = np.power(zol, 2)/(1+np.power(zol, 2))
psi = np.where(zol < 0, (1-f)*psik+f*psic, psi)
return psi
# ---------------------------------------------------------------------
def psi_conv(zol, alpha, beta, gamma):
""" Calculates heat stability function for unstable conditions
Parameters
----------
zol : float
height over MO length
alpha, beta, gamma : float
constants given by get_stabco
Returns
-------
psit : float
"""
xtmp = (1-alpha*zol)**beta
psit = 2*np.log((1+xtmp**2)*0.5)
return psit
# ---------------------------------------------------------------------
def psi_stab(zol, alpha, beta, gamma):
""" Calculates heat stability function for stable conditions
Parameters
----------
zol : float
height over MO length
alpha, beta, gamma : float
constants given by get_stabco
Returns
-------
psit : float
"""
psit = -gamma*zol
return psit
# ---------------------------------------------------------------------
def psim_stab_era5(zol, alpha, beta, gamma):
""" Calculates momentum stability function for stable conditions
for method ERA5
Parameters
----------
zol : float
height over MO length
alpha, beta, gamma : float
constants given by get_stabco
Returns
-------
psim : float
"""
# eq (3.22) p. 39 IFS Documentation cy46r1
a, b, c, d = 1, 2/3, 5, 0.35
psim = -b*(zol-c/d)*np.exp(-d*zol)-a*zol-(b*c)/d
return psim
# ---------------------------------------------------------------------
def psim_conv(zol, alpha, beta, gamma):
""" Calculates momentum stability function for unstable conditions
Parameters
----------
zol : float
height over MO length
alpha, beta, gamma : float
constants given by get_stabco
Returns
-------
psim : float
"""
xtmp = (1-alpha*zol)**beta
psim = (2*np.log((1+xtmp)*0.5)+np.log((1+xtmp**2)*0.5) -
2*np.arctan(xtmp)+np.pi/2)
return psim
# ---------------------------------------------------------------------
def psim_stab(zol, alpha, beta, gamma):
""" Calculates momentum stability function for stable conditions
Parameters
----------
zol : float
height over MO length
alpha, beta, gamma : float
constants given by get_stabco
Returns
-------
psim : float
"""
psim = -gamma*zol
return psim
# ---------------------------------------------------------------------
def psiu_26(zol, meth):
""" Computes velocity structure function C35
Parameters
----------
zol : float
height over MO length
Returns
-------
psi : float
"""
if (meth == "C30"):
dzol = np.where(0.35*zol > 50, 50, 0.35*zol) # stable
psi = -((1+zol)+0.6667*(zol-14.28)*np.exp(-dzol)+8.525)
k = np.where(zol < 0) # unstable
x = np.power(1-15*zol[k], 0.25)
psik = (2*np.log((1+x)/2)+np.log((1+np.power(x, 2))/2)-2*np.arctan(x) +
2*np.arctan(1))
x = np.power(1-10.15*zol[k], 0.3333)
psic = (1.5*np.log((1+x+np.power(x, 2))/3)-np.sqrt(3) *
np.arctan((1+2*x)/np.sqrt(3))+4*np.arctan(1)/np.sqrt(3))
f = np.power(zol[k], 2)/(1+np.power(zol[k], 2))
psi[k] = (1-f)*psik+f*psic
elif (meth == "C35" or meth == "C40"):
dzol = np.where(0.35*zol > 50, 50, 0.35*zol) # stable
a, b, c, d = 0.7, 3/4, 5, 0.35
psi = -(a*zol+b*(zol-c/d)*np.exp(-dzol)+b*c/d)
k = np.where(zol < 0) # unstable
x = np.power(1-15*zol[k], 0.25)
psik = 2*np.log((1+x)/2)+np.log((1+x**2)/2)-2*np.arctan(x)+2*np.arctan(1)
x = np.power(1-10.15*zol[k], 0.3333)
psic = (1.5*np.log((1+x+np.power(x, 2))/3)-np.sqrt(3) *
np.arctan((1+2*x)/np.sqrt(3))+4*np.arctan(1)/np.sqrt(3))
f = np.power(zol[k], 2)/(1+np.power(zol[k], 2))
psi[k] = (1-f)*psik+f*psic
return psi
# ------------------------------------------------------------------------------
def psiu_40(zol):
""" Computes velocity structure function C35
Parameters
----------
zol : float
height over MO length
Returns
-------
psi : float
"""
dzol = np.where(0.35*zol > 50, 50, 0.35*zol) # stable
a, b, c, d = 1, 3/4, 5, 0.35
psi = -(a*zol+b*(zol-c/d)*np.exp(-dzol)+b*c/d)
k = np.where(zol < 0) # unstable
x = (1-18*zol[k])**0.25
psik = 2*np.log((1+x)/2)+np.log((1+x**2)/2)-2*np.arctan(x)+2*np.arctan(1)
x = (1-10*zol[k])**0.3333
psic = (1.5*np.log((1+x+x**2)/3)-np.sqrt(3)*np.arctan((1+2*x)/np.sqrt(3)) +
4*np.arctan(1)/np.sqrt(3))
f = zol[k]**2/(1+zol[k]**2)
psi[k] = (1-f)*psik+f*psic
return psi
# ---------------------------------------------------------------------
def get_skin(sst, qsea, rho, Rl, Rs, Rnl, cp, lv, tkt, usr, tsr, qsr, lat):
""" Computes cool skin
Parameters
----------
sst : float
sea surface temperature ($^\circ$\,C)
qsea : float
specific humidity over sea (g/kg)
rho : float
density of air (kg/m^3)
Rl : float
downward longwave radiation (W/m^2)
Rs : float
downward shortwave radiation (W/m^2)
Rnl : float
upwelling IR radiation (W/m^2)
cp : float
specific heat of air at constant pressure
lv : float
latent heat of vaporization
tkt : float
cool skin thickness
usr : float
friction velocity
tsr : float
star temperature
qsr : float
star humidity
lat : float
latitude
Returns
-------
dter : float
dqer : float
"""
# coded following Saunders (1967) with lambda = 6
g = gc(lat, None)
if (np.nanmin(sst) > 200): # if Ta in Kelvin convert to Celsius
sst = sst-273.16
# ************ cool skin constants *******
# density of water, specific heat capacity of water, water viscosity,
# thermal conductivity of water
rhow, cpw, visw, tcw = 1022, 4000, 1e-6, 0.6
Al = 2.1e-5*np.power(sst+3.2, 0.79)
be = 0.026
bigc = 16*g*cpw*np.power(rhow*visw, 3)/(np.power(tcw, 2)*np.power(rho, 2))
wetc = 0.622*lv*qsea/(287.1*np.power(sst+273.16, 2))
Rns = 0.945*Rs # albedo correction
hsb = -rho*cp*usr*tsr
hlb = -rho*lv*usr*qsr
qout = Rnl+hsb+hlb
dels = Rns*(0.065+11*tkt-6.6e-5/tkt*(1-np.exp(-tkt/8.0e-4)))
qcol = qout-dels
alq = Al*qcol+be*hlb*cpw/lv
xlamx = 6*np.ones(sst.shape)
xlamx = np.where(alq > 0, 6/(1+(bigc*alq/usr**4)**0.75)**0.333, 6)
tkt = np.where(alq > 0, xlamx*visw/(np.sqrt(rho/rhow)*usr),
np.where(xlamx*visw/(np.sqrt(rho/rhow)*usr) > 0.01, 0.01,
xlamx*visw/(np.sqrt(rho/rhow)*usr)))
dter = qcol*tkt/tcw
dqer = wetc*dter
return dter, dqer, tkt
# ---------------------------------------------------------------------
def get_gust(beta, Ta, usr, tsrv, zi, lat):
""" Computes gustiness
Parameters
----------
beta : float
constant
Ta : float
air temperature (K)
usr : float
friction velocity (m/s)
tsrv : float
star virtual temperature of air (K)
zi : int
scale height of the boundary layer depth (m)
lat : float
latitude
Returns
-------
ug : float
"""
if (np.nanmax(Ta) < 200): # convert to K if in Celsius
Ta = Ta+273.16
g = gc(lat, None)
Bf = (-g/Ta)*usr*tsrv
ug = np.ones(np.shape(Ta))*0.2
ug = np.where(Bf > 0, beta*np.power(Bf*zi, 1/3), 0.2)
return ug
# ---------------------------------------------------------------------
def get_heights(h):
""" Reads input heights for velocity, temperature and humidity
Parameters
----------
h : float
input heights (m)
Returns
-------
hh : array
"""
hh = np.zeros(3)
if (type(h) == float or type(h) == int):
hh[0], hh[1], hh[2] = h, h, h
elif len(h) == 2:
hh[0], hh[1], hh[2] = h[0], h[1], h[1]
else:
hh[0], hh[1], hh[2] = h[0], h[1], h[2]
return hh
# ---------------------------------------------------------------------
def svp_calc(T):
""" Calculates saturation vapour pressure
Parameters
----------
T : float
temperature (K)
Returns
-------
svp : float
in mb, pure water
"""
if (np.nanmin(T) < 200): # if T in Celsius convert to Kelvin
T = T+273.16
svp = np.where(np.isnan(T), np.nan, 2.1718e08*np.exp(-4157/(T-33.91-0.16)))
return svp
# ---------------------------------------------------------------------
def qsea_calc(sst, pres):
""" Computes specific humidity of the sea surface air
Parameters
----------
sst : float
sea surface temperature (K)
pres : float
pressure (mb)
Returns
-------
qsea : float
(kg/kg)
"""
if (np.nanmin(sst) < 200): # if sst in Celsius convert to Kelvin
sst = sst+273.16
ed = svp_calc(sst)
e = 0.98*ed
qsea = (0.622*e)/(pres-0.378*e)
qsea = np.where(~np.isnan(sst+pres), qsea, np.nan)
return qsea
# ---------------------------------------------------------------------
def q_calc(Ta, rh, pres):
""" Computes specific humidity following Haltiner and Martin p.24
Parameters
----------
Ta : float
air temperature (K)
rh : float
relative humidity (%)
pres : float
air pressure (mb)
Returns
-------
qair : float, (kg/kg)
"""
if (np.nanmin(Ta) < 200): # if sst in Celsius convert to Kelvin
Ta = Ta+273.15
e = np.where(np.isnan(Ta+rh+pres), np.nan, svp_calc(Ta)*rh*0.01)
qair = np.where(np.isnan(e), np.nan, ((0.62197*e)/(pres-0.378*e)))
return qair
# ------------------------------------------------------------------------------
def bucksat(T, P):
""" Computes saturation vapor pressure (mb) as in C35
Parameters
----------
T : float
temperature ($^\\circ$\\,C)
P : float
pressure (mb)
Returns
-------
exx : float
"""
T = np.asarray(T)
if (np.nanmin(T) > 200): # if Ta in Kelvin convert to Celsius
T = T-CtoK
exx = 6.1121*np.exp(17.502*T/(T+240.97))*(1.0007+3.46e-6*P)
return exx
# ------------------------------------------------------------------------------
def qsat26sea(T, P):
""" Computes surface saturation specific humidity (g/kg) as in C35
Parameters
----------
T : float
temperature ($^\\circ$\\,C)
P : float
pressure (mb)
Returns
-------
qs : float
"""
T = np.asarray(T)
if (np.nanmin(T) > 200): # if Ta in Kelvin convert to Celsius
T = T-CtoK
ex = bucksat(T, P)
es = 0.98*ex # reduction at sea surface
qs = 622*es/(P-0.378*es)
return qs
# ------------------------------------------------------------------------------
def qsat26air(T, P, rh):
""" Computes saturation specific humidity (g/kg) as in C35
Parameters
----------
T : float
temperature ($^\circ$\,C)
P : float
pressure (mb)
Returns
-------
q : float
em : float
"""
T = np.asarray(T)
if (np.nanmin(T) > 200): # if Ta in Kelvin convert to Celsius
T = T-CtoK
es = bucksat(T, P)
em = 0.01*rh*es
q = 622*em/(P-0.378*em)
return q, em
# ---------------------------------------------------------------------
def gc(lat, lon=None):
""" Computes gravity relative to latitude
Parameters
----------
lat : float
latitude ($^\circ$)
lon : float
longitude ($^\circ$, optional)
Returns
-------
gc : float
gravity constant (m/s^2)
"""
gamma = 9.7803267715
c1 = 0.0052790414
c2 = 0.0000232718
c3 = 0.0000001262
c4 = 0.0000000007
if lon is not None:
lon_m, lat_m = np.meshgrid(lon, lat)
else:
lat_m = lat
phi = lat_m*np.pi/180.
xx = np.sin(phi)
gc = (gamma*(1+c1*np.power(xx, 2)+c2*np.power(xx, 4)+c3*np.power(xx, 6) +
c4*np.power(xx, 8)))
return gc
# ---------------------------------------------------------------------
def visc_air(T):
""" Computes the kinematic viscosity of dry air as a function of air temp.
following Andreas (1989), CRREL Report 89-11.
Parameters
----------
Ta : float
air temperature ($^\circ$\,C)
Returns
-------
visa : float
kinematic viscosity (m^2/s)
"""
T = np.asarray(T)
if (np.nanmin(T) > 200): # if Ta in Kelvin convert to Celsius
T = T-273.16
visa = 1.326e-5*(1+6.542e-3*T+8.301e-6*np.power(T, 2) -
4.84e-9*np.power(T, 3))
return visa