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KLModels.py
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302 lines (222 loc) · 8.74 KB
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"""
----------------------------------
Turbulence models
MSc Project @ Reading:
Somrath Kanoksirirath
StudentID 26835996
----------------------------------
KLModels.py = some implementations of k-l turbulence model
- MSC
- KNMI_RACMO
- NASA
- YorkU1
- YorkU2
- LouvainUL
----------------------------------
Copyright (c) 2019, Somrath Kanoksirirath.
All rights reserved under BSD 3-clause license.
"""
import numpy as np
from abstractModels import Setup, KL_model
from BC import Boundary_Cuxart2006 as defaultBC
class MSC(KL_model):
"""
MSC k-l turbulence model (Belair et al., 1999)
(derived from "KL_model_S" class)
"""
def __init__(self, dt=10., nz=64, Lz=400.,
BC=defaultBC(), para=Setup(), scheme=2):
KL_model.__init__(self, dt, nz, Lz, BC, para, scheme)
self.__lm = np.minimum(self.BC.k*self.z_secondary[:-1], 200.)
# (Pseudo) Protected functions:
def _get_c(self):
"Return [cm, ch, ce, deps]"
return [0.516, 0.516/0.85, 1.0, 0.14] # ceps in stable (Mailhot, 1982)
def _get_l_and_f(self):
"Return [lm, lh, leps, fm, fh]"
# Ri <-- from Reference paper
dudz = self.grad_PtoS(self.u)
dvdz = self.grad_PtoS(self.v)
dUdz2 = np.power(dudz, 2) + np.power(dvdz, 2)
dUdz2 = np.maximum(dUdz2, 1e-12)
dTdz = self.grad_PtoS(self.T)
Ri = np.divide(self.para.g*dTdz/self.para.T_ref, dUdz2)
# Ri_f
S = np.multiply(self.uw[:-1], dudz) + np.multiply(self.vw[:-1], dvdz)
S = np.maximum(S, 1e-12)
Rif = np.divide(self.para.g*self.wT[:-1]/self.para.T_ref, S)
### For both stable (Ri>0) and unstable (Ri<0)
fm = np.zeros_like(Ri)
# Stable
mask = Ri > 0.
fm[mask] = 1./(1. + 12.*Ri[mask])
# Unstable
mask = np.logical_not(mask)
fm[mask] = np.power(1. - 40.*Ri[mask], 1./6.)
feps = np.ones_like(Ri)
mask = Rif < 0.4
feps[mask] = np.divide(1.-Rif[mask], 1.-2.*Rif[mask])
feps[np.logical_not(mask)] = 3.
return [self.__lm, self.__lm, np.multiply(self.__lm, feps), fm, fm]
class KNMI_RACMO(KL_model):
"""
KNMI-RACMO k-l turbulence model (Lenderink and Holtslay, 2004)
(derived from "KL_model_S" class)
"""
def __init__(self, dt=10., nz=64, Lz=400.,
BC=defaultBC(), para=Setup(), scheme=2):
KL_model.__init__(self, dt, nz, Lz, BC, para, scheme)
self.__lm = 1./(1./self.BC.k/self.z_secondary[:-1] + 1./150.)
# (Pseudo) Protected functions:
def _get_c(self):
"Return [cm, ch, ce, deps]"
return [0.4868546887, 0.6985192675, 2., 0.071111111111/0.4868546887]
def _get_l_and_f(self):
"Return [lm, lh, leps, fm, fh]"
dudz = self.grad_PtoS(self.u)
dvdz = self.grad_PtoS(self.v)
dUdz2 = np.power(dudz, 2) + np.power(dvdz, 2)
dUdz2 = np.maximum(dUdz2, 1e-12)
dTdz = self.grad_PtoS(self.T)
Ri = np.divide(self.para.g*dTdz/self.para.T_ref, dUdz2)
# For stable (Ri>0) ONLY
if np.any(Ri < 0) :
print('This model is not for unstable cases yet.')
temp = np.sqrt(1. + 5.*Ri)
fm = 1./(1. + 10.*np.divide(Ri, temp))
fh = 1./(1. + 15.*np.multiply(Ri, temp))
return [self.__lm, self.__lm, self.__lm, fm, fh]
class NASA(KL_model):
"""
NASA k-l turbulence model (see Moeng, 1984)
(derived from "KL_model_S" class)
"""
def __init__(self, dt=10., nz=64, Lz=400.,
BC=defaultBC(), para=Setup(), scheme=2):
KL_model.__init__(self, dt, nz, Lz, BC, para, scheme)
# (Pseudo) Protected functions:
def _get_c(self):
"Return [cm, ch, ce, deps]"
return [0.1, 0.1, 2., 1.]
def _get_l_and_f(self):
"Return [lm, lh, leps, fm, fh]"
# For both stable (Ri>0) and unstable (Ri<0) ?
Stra = self.para.g*self.grad_PtoS(self.T)/self.para.T_ref
# Stable
lm = np.ones_like(Stra)
mask = Stra > 0
Stra[mask] = np.maximum(Stra[mask], 1e-12)
lm[mask] = 0.76*np.sqrt(np.divide(self.TKE[mask], Stra[mask]))
# Unstable
mask = np.logical_not(mask)
lm[mask] = 2*self._dz
lm = np.minimum(lm, 2*self._dz) # 2, because of staggered grid?
lh = np.multiply(np.minimum(1. + 2.*lm/self._dz, 3.), lm)
leps = np.divide(lm, 0.19 + 0.51*lm/self._dz)
return [lm, lh, leps, np.ones_like(lm), np.ones_like(lm)]
class YorkU1(KL_model):
"""
1st York University k-l turbulence model (Weng and Taylor, 2003)
(derived from "KL_model_S" class)
"""
def __init__(self, dt=10., nz=64, Lz=400.,
BC=defaultBC(), para=Setup(), scheme=2):
KL_model.__init__(self, dt, nz, Lz, BC, para, scheme)
# (Pseudo) Protected functions:
def _get_c(self):
"Return [cm, ch, ce, deps]"
#return [0.55, 0.55/0.85, 1., 1.] # Cuxart et al (2006)
cm = (self.BC.cn)**-0.5
return [cm, cm/0.85, 1., cm**3] # Weng and Taylor (2003) and our BC
def _get_l_and_f(self):
"Return [lm, lh, leps, fm, fh]"
# For both stable (Ri>0) and unstable (Ri<0)
Stra = self.para.g*self.grad_PtoS(self.T)/self.para.T_ref
### Find lnc
# 1. rl0 = 1./l0
rl0 = self.para.f/0.0027/np.sqrt(self.para.Ug**2 + self.para.Vg**2)
# 2. rlz = phiM/k(z+z0)
# Assume BC.L>0 for phiM
if self.BC.rL > 0 :
phiM = 1. + 4.7*self.BC.rL*self.z_secondary[:-1]
else:
phiM = np.power(1. - 15*self.BC.rL*self.z_secondary[:-1], 0.25)
rlz = np.divide(phiM, self.BC.k*(self.z_secondary[:-1] + self.z_primary[0]))
# 3. lnc =
lnc = 1./(rlz + rl0)
### Find lm
lm = np.zeros_like(Stra)
# Stable
mask = Stra > 0
Stra[mask] = np.maximum(Stra[mask], 1e-12)
lm[mask] = np.minimum(lnc[mask],
0.36*np.sqrt(np.divide(self.TKE[mask], Stra[mask])))
# Unstable
mask = np.logical_not(mask)
lm[mask] = lnc[mask]
return [lm, lm, lm, np.ones_like(lm), np.ones_like(lm)]
class YorkU2(KL_model):
"""
2nd York University k-l turbulence model
(Weng and Taylor, 2003) + (Delage, 1974)
(derived from "KL_model_S" class)
"""
def __init__(self, dt=10., nz=64, Lz=400.,
BC=defaultBC(), para=Setup(), scheme=2):
KL_model.__init__(self, dt, nz, Lz, BC, para, scheme)
# (Pseudo) Protected functions:
def _get_c(self):
"Return [cm, ch, ce, deps]"
#return [0.55, 0.55/0.85, 1., 1.] # Cuxart et al (2006)
cm = (self.BC.cn)**-0.5
return [cm, cm/0.85, 1., cm**3] # Weng and Taylor (2003) and our BC
def _get_l_and_f(self):
"Return [lm, lh, leps, fm, fh]"
# For both stable (Ri>0) and unstable (Ri<0)
if np.any(self.grad_PtoS(self.T) < 0) :
print('This model is not for unstable cases yet.')
### Find lnc
# 1. rl0 = 1./l0
rl0 = self.para.f/0.0027/np.sqrt(self.para.Ug**2 + self.para.Vg**2)
# 2. rlz = phiM/k(z+z0)
# Assume BC.L>0 for phiM
if self.BC.rL > 0 :
phiM = 1. + 4.7*self.BC.rL*self.z_secondary[:-1]
else:
phiM = np.power(1. - 15*self.BC.rL*self.z_secondary[:-1], 0.25)
rlz = np.divide(phiM, self.BC.k*(self.z_secondary[:-1] + self.z_primary[0]))
# Find lm (stable case only)
lm = 1./(rlz + rl0 + 4.7*self.BC.rL/0.4)
leps = 1./(rlz + rl0 + 3.7*self.BC.rL/0.4)
return [lm, lm, leps, np.ones_like(lm), np.ones_like(lm)]
class LouvainUL(KL_model):
"""
Louvain University k-l turbulence model
(derived from "KL_model_S" class)
"""
def __init__(self, dt=10., nz=64, Lz=400.,
BC=defaultBC(), para=Setup(), scheme=2):
KL_model.__init__(self, dt, nz, Lz, BC, para, scheme)
# (Pseudo) Protected functions:
def _get_c(self):
"Return [cm, ch, ce, deps]"
return [0.5, 1.3*0.5, 1., 0.125] # ce is guessed.
def _get_l_and_f(self):
"Return [lm, lh, leps, fm, fh]"
### For stable case (Ri>0) ONLY
# 1. Find lz
lz = self.BC.k*self.z_secondary[:-1]
# 2. Find lsurface
lsur = 0.3*self.BC.u_star/self.para.f
# 3. Find ls
Stra = self.para.g*self.grad_PtoS(self.T)/self.para.T_ref
if np.any(Stra < 0) :
print('This model is not for unstable cases yet.')
ls = np.zeros_like(Stra)
mask = Stra > 0
ls[mask] = np.sqrt(self.TKE[mask]/Stra[mask])
ls[np.logical_not(mask)] = float('inf')
# 4. Find lm, leps
lm = 1./(1./lz + 15./lsur + 1.5/ls)
leps = 1./(1./lz + 15./lsur + 3./ls)
return [lm, lm, leps, np.ones_like(lm), np.ones_like(lm)]