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Comparing $\overline{w'w'}$ and $\overline{w'w'w'}$ tendency terms between ADC and LES #13

@BrodiePearson

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@BrodiePearson

This issue lists the ADC tendency terms for $\overline{w'w'}$ and $\overline{w'w'w'}$, and the analogous LES terms (where possible).

One avenue for diagnosing the skill of the ADC closure scheme is to compare whether the tendency terms in the scheme are comparable to LES data. The tendency terms in the ADC and LES schemes represent similar physical processes, but because the ADC scheme has closure assumptions that are distinct from Reynolds averaging (which is how we analyze LES fields), the tendency terms in the ADC and LES schemes differ in their form.

$\overline{w'w'}$ budget

w2tend1(k,iCell) = -wumd(k,iCell)**2.0_RKIND*( &
Entrainment(k,iCell) + Detrainment(k,iCell))

$w2tend1=$? (Entrainment/Detrainment; maybe dissipation related or this doesn't have an LES analogy)

w2tend2(k,iCell) = (McMid(k-1,iCell)*(1.0_RKIND - 2.0_RKIND* &
areaFractionMid(k-1,iCell))*wumdMid(k-1,iCell)**2.0 - McMid(k,iCell)* &
(1.0_RKIND - 2.0_RKIND*areaFractionMid(k,iCell))*wumdMid(k,iCell)**2.0) / dzmid

$w2tend2=-\frac{\partial \overline{w'w'w'}}{\partial z}$ (Turbulent transport)

w2tend3(k,iCell) = tauvVel(k,iCell)*(u2(i1,k,iCell) + v2(i1,k,iCell))/3.0_RKIND

$w2tend3=\frac{ \overline{u'u'} + \overline{v'v'} }{3\tau_{slow}}$ (Part of slow pressure; a missing $\overline{w'w'}$ term is added in time-stepping)

w2tend4(k,iCell) = (2.0_RKIND - 4.0_RKIND/3.0_RKIND*C_2)*Mc(k,iCell)* &
(grav*alphaT(k,iCell)*tumd(k,iCell) - grav*betaS(k,iCell)*sumd(k,iCell))

$w2tend4= ( 2 - \frac{4}{3}C_2 ) \overline{w'b'} = ( 2 - \frac{4}{3}C_2 ) g ( \alpha_T \overline{w'T'} - \beta_S \overline{w'S'} )$ (Buoyancy plus buoyancy pressure term)

w2tend5(k,iCell) = (1.0_RKIND/3.0_RKIND*alpha1 - &
alpha2)*(uw(i1,k,iCell)*Uz + vw(i1,k,iCell)*Vz) + &
Mc(k,iCell)*(Swumd(k-1,iCell) + Swumd(k,iCell))

$w2tend5= complicated$ (Rapid pressure & subgrid terms, dissipation too(?))

w2tend6(k,iCell) = min(max(-config_adc_splat_tend_max, -w2(i1,k,iCell)* &
config_adc_splat_wp2_val*tau_sfc*d_sqrt_wp2_dz**2), &
config_adc_splat_tend_max)

$w2tend6= Splatting$ (Effectively a pressure term that converts w2 to u2 and v2 near the surface)

We could add a combined pressure term that is only used for comparison with LES: w2tend_pressure $= w2tend3 + w2tend5 + w2tend6 - \frac{2\overline{w'w'}}{3\tau_{slow}} - \frac{\frac{4}{3}C_2}{2-\frac{4}{3}C_2} w2tend4$

Then, $w2tend$_$pressure \approx -2\overline{w'\frac{\partial p'}{\partial z}}$

Since $w2tend5$ also contains dissipation, perhaps we go one step further by combining pressure and dissipation terms

$w2tend1 + w2tend$_$pressure = -2\overline{w'\frac{\partial p'}{\partial z}} - \frac{2}{3}\epsilon $

$\overline{w'w'w'}$ budget

w3tend1(k,iCell) = -wumdav**3.0*(Eav*(3.0*sigav - 2.0) + Dav*(3.0*sigav - 1.0))

$w3tend1=?$ (Entrainment/Detrainment - perhaps analogous to LES dissipation of $\overline{w'w'w'}$)

w3tend2(k,iCell) = -((3.0_RKIND + Swk**2.0)*(w2(i1,k,iCell)**2.0) - &
(3.0_RKIND + Swk**2.0)*(w2(i1,k+1,iCell)**2.0) ) / dz

$w3tend2=-\frac{\partial \overline{w'w'w'w'}}{\partial z}$ (Turbulent transport, the 4th moment may not be LES output...)

w3tend3(k,iCell) = 1.5_RKIND*(w2(i1,k,iCell)**2.0 - w2(i1,k+1,iCell)**2.0) / dz

$w3tend3=\frac{3}{2}\frac{\partial \left[ \left(\overline{w'w'}\right)^2 \right]}{\partial z}$ (Source term from w2 gradients)

w3tend4(k,iCell) = -3.0_RKIND*(1.0_RKIND - 2.0_RKIND*sigav)*Mcav*wumdav*Swumd(k,iCell) - &
tauw3(k,iCell)*w3(i1,k,iCell)

$w3tend4=complicated$ (Sub-plume scale transport and slow pressure term)

w3tend5(k,iCell) = 3.0_RKIND*(1.0_RKIND - c11)*grav*(alphaT(k,iCell)*w2t(k,iCell) - &
betaS(k,iCell)*w2s(k,iCell))

$w3tend5=3(1-C_{11})\overline{w'w'b'}$ (Buoyancy production plus buoyancy pressure term)

w3tend6(1,iCell) = min(max(-config_adc_splat_tend_max, -w3(i1,1,iCell)* &
config_adc_splat_wp2_val*tau_sfc*d_sqrt_wp2_dz**2), &
config_adc_splat_tend_max)

$w3tend6=Splatting$ (This is effectively a pressure-driven effect)

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