TrioCFD 1.9.8
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Diffu_lm.cpp
1/****************************************************************************
2* Copyright (c) 2015 - 2016, CEA
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15
16#include <Diffu_lm.h>
17#include <Fluide_base.h>
18#include <MuLambda_TBLE_base.h>
19
20Implemente_instanciable(Diffu_lm,"Diffu_lm",Diffu_totale_hyd_base);
21
22
23const double Diffu_lm::A_plus=25.;
24
26{
27 return os ;
28}
29
31{
32 return is ;
33}
34
35//////////////////////////////////////////////////////////////////////////////////////////////////////////
36//// Cette methode determine la diffusivite totale a en un point donne du maillage fin de Eq_couch_lim ///
37//////////////////////////////////////////////////////////////////////////////////////////////////////////
38
39// Si la composante du cisaillement a la paroi est dans le sens de l'ecoulement
40
42{
43 // OC : 02/2006 ; on pourrait peut etre remplacer ce "calculer_a_local" par un "calculer_a_global", ce qui eviterait de multiples appels, surement couteux, a cette methode.
44
45 double yw, y_plus, a, Damp, S_norm ;
46 double yw_N, y_plus_N, S_norm_N, Damp_N ;
47
48 //S_norm est la norme de Sij sur le maillage fin
49 //Damp est une fonction de damping
50 //u_tau : vitesse de frottement
51
52 int N;
53 double kappa = -123;
54 Eq_couch_lim& leq = eq_couch_lim.valeur();
55 double visco_cin = mu_lambda->getNu(eq_couch_lim_T, ind);
56 double visco_cin2 = mu_lambda->getNu(eq_couch_lim_T, ind+1);
57 double visco_turb = 0.;
58 int nb_comp = leq.get_N_comp();
59
60
61 N = leq.get_N();
62
63 yw = 0.5*(leq.get_y(ind+1)+leq.get_y(ind));
64 y_plus = yw*leq.get_utau_old()/(0.5*(visco_cin+visco_cin2));
65 Damp = 1-exp(pow(-y_plus/A_plus,3)); // Damp1
66 //Damp = pow(1-exp(-y_plus/A_plus),2); // Damp2
67
68 if(leq.get_nu_t_dyn() == 0)
69 {
70 kappa=getKappa();
71 }
72 else
73 {
74 double visco_cin_N = 0.5*(mu_lambda->getNu(eq_couch_lim_T, N-1)+mu_lambda->getNu(eq_couch_lim_T, N));
75 yw_N = 0.5*(leq.get_y(N)+leq.get_y(N-1));
76 y_plus_N = yw_N*leq.get_utau_old()/visco_cin_N;
77 //Damp_N = 1-exp(pow(-y_plus_N/A_plus,3)); // Damp1
78 Damp_N = pow(1-exp(-y_plus_N/A_plus),2); // Damp2
79
80 S_norm_N = 0.;
81 double tmp=0.;
82 for (int icomp=0; icomp<nb_comp; icomp++)
83 {
84 tmp = (leq.get_Unp1(icomp,N) - leq.get_Unp1(icomp,N-1))/(leq.get_y(N)-leq.get_y(N-1));
85 S_norm_N += tmp*tmp;
86 }
87 S_norm_N=sqrt(S_norm_N);
88 // kappa = (1./yw_N)*sqrt(leq.get_nu_t_yn()/(Damp_N*S_norm_N));
89 kappa = leq.get_nu_t_yn()/(y_plus_N*visco_cin_N*Damp_N);
90
91 if(kappa > getKappa())
92 kappa = getKappa();
93 else if(kappa < 0.)
94 kappa = 0;
95 }
96
97 if(ind==0)
98 {
99 a = visco_cin;
100 }
101 else
102 {
103 //Norme de Sij
104 S_norm = 0.;
105 double tmp=0.;
106 for (int icomp=0; icomp<nb_comp; icomp++)
107 {
108 tmp = (leq.get_Unp1(icomp,ind+1) - leq.get_Unp1(icomp,ind))/(leq.get_y(ind+1)-leq.get_y(ind));
109 S_norm += tmp*tmp;
110 }
111 S_norm=sqrt(S_norm);
112
113 visco_turb = kappa*kappa*yw*yw*S_norm*Damp;
114 //visco_turb = kappa*y_plus*visco_cin*Damp;
115 a = visco_cin + visco_turb;
116 }
117 return a;
118}
119
120/////////////////////////////////////////////////////////////////////////////////////
121// //
122// La viscosite turbulente est calculee grace a un modele de longueur de melange ://
123// nu_t = (kappa*y)^2*Damp*|S| //
124// Cette formulation est proposee dans l'article de Balaras et al. //
125// AIAA journal vol. 34, no 6, 1996 //
126// //
127/////////////////////////////////////////////////////////////////////////////////////
128
129//////////////////////////////////////////////
130//Calcul de la fonction de damping uniquement
131//Attention : Ne pas integrer !!!
132//////////////////////////////////////////////
134{
135
136 double yw, y_plus, Damp ;
137
138 //Damp est une fonction de damping
139 //u_tau : vitesse de frottement
140
141
142 Eq_couch_lim& leq = eq_couch_lim.valeur();
143 const Milieu_base& le_milieu = leq.get_milieu();
144 const Fluide_base& le_fluide = ref_cast(Fluide_base, le_milieu);
145 const Champ_Don_base& ch_visco_cin = le_fluide.viscosite_cinematique();
146 const DoubleTab& tab_visco = ch_visco_cin.valeurs();
147
148 double visco_cin = std::max(tab_visco(0,0),DMINFLOAT);//visco cinematique supposee cste
149
150 yw = 0.5*(leq.get_y(ind+1)+leq.get_y(ind));
151 y_plus = yw*leq.get_utau_old()/visco_cin;
152 Damp = 1-exp(pow(-y_plus/A_plus,3)); // Damp1
153
154 return Damp;
155}
classe Champ_Don_base classe de base des Champs donnes (non calcules)
DoubleTab & valeurs() override
Surcharge Champ_base::valeurs() Renvoie le tableau des valeurs.
Classe Diffu_lm Calsse derivant de la classe Diffu_totale_hyd__base et specifiant la valeur.
Definition Diffu_lm.h:31
double calculer_a_local(int ind) override
Definition Diffu_lm.cpp:41
double calculer_D_local(int ind) override
Definition Diffu_lm.cpp:133
Classe Diffu_totale_hyd_base Classe abstraite calculant la diffusivite totale (somme diffusivite.
Class defining operators and methods for all reading operation in an input flow (file,...
Definition Entree.h:42
double get_nu_t_yn()
double get_y(int i)
double get_Unp1(int j, int i)
double get_nu_t_dyn()
double get_utau_old()
Milieu_base & get_milieu()
classe Fluide_base Cette classe represente un d'un fluide incompressible ainsi que
Definition Fluide_base.h:38
const Champ_Don_base & viscosite_cinematique() const
Definition Fluide_base.h:58
classe Milieu_base Cette classe est la base de la hierarchie des milieux (physiques)
Definition Milieu_base.h:50
virtual Entree & readOn(Entree &)
Lecture d'un Objet_U sur un flot d'entree Methode a surcharger.
Definition Objet_U.cpp:293
virtual Sortie & printOn(Sortie &) const
Ecriture de l'objet sur un flot de sortie Methode a surcharger.
Definition Objet_U.cpp:282
Classe de base des flux de sortie.
Definition Sortie.h:52