EsatCV=2⋅VSATCV(T)⋅Dmob,cvμ0(T)(3.403) E_{satCV} = \dfrac{2 \cdot VSATCV(T) \cdot D_{mob,cv}}{\mu_0(T)} \qquad (3.403) EsatCV=μ0(T)2⋅VSATCV(T)⋅Dmob,cv(3.403)
EsatCVL=EsatCV⋅LeffCV(3.404) E_{satCVL} = E_{satCV} \cdot L_{effCV} \qquad (3.404) EsatCVL=EsatCV⋅LeffCV(3.404)
Dvsat,CV=1+[δvsat,cv+(ΔqiEsatCVL)PSATCV(L)]1PSATCV(L)1+(δvsat,cv)1PSATCV(L)(3.405) D_{vsat,CV} = \dfrac{1 + \Big[ \delta_{vsat,cv} + \Big( \frac{\Delta q_i}{E_{satCVL}} \Big)^{PSATCV(L)} \Big]^{\frac{1}{PSATCV(L)}}}{1 + (\delta_{vsat,cv})^{\frac{1}{PSATCV(L)}}} \qquad (3.405) Dvsat,CV=1+(δvsat,cv)PSATCV(L)11+[δvsat,cv+(EsatCVLΔqi)PSATCV(L)]PSATCV(L)1(3.405)