예제 #1
0
        public static Capiliary_res CapiliaryCalc(int index, string fluid, double d_cap, double lenth_cap, double tri, double pri, double hri, double mr, double Pwater, int hexType, AbstractState coolprop, double[,] SourceTableData)
        {
            //毛细管守恒方程模型
            //AbstractState coolprop = AbstractState.factory("HEOS", fluid);

            Capiliary_res res_cap = new Capiliary_res();

            double Ar_cs = Math.PI * Math.Pow(d_cap, 2) / 4;
            double g     = mr / Ar_cs;

            coolprop.update(input_pairs.PQ_INPUTS, pri * 1000, 0);
            double tsat = coolprop.T();

            //double tsat = CoolProp.PropsSI("T", "P", pri * 1000, "Q", 0, fluid);
            coolprop.update(input_pairs.QT_INPUTS, 0, tsat);
            double h_l = coolprop.hmass() / 1000;

            //double h_l = CoolProp.PropsSI("H", "T", tsat, "Q", 0, fluid) / 1000;
            coolprop.update(input_pairs.QT_INPUTS, 1, tsat);
            double h_v = coolprop.hmass() / 1000;
            //double h_v = CoolProp.PropsSI("H", "T", tsat, "Q", 1, fluid) / 1000;

            double x_i = (hri - h_l) / (h_v - h_l);

            coolprop.update(input_pairs.PQ_INPUTS, (fluid == "Water" ? Pwater : pri) * 1000, 1);
            double rho_gi = coolprop.rhomass();

            //double rho_gi = CoolProp.PropsSI("D", "Q", 1, "P", (fluid == "Water" ? Pwater : pri) * 1000, fluid);
            coolprop.update(input_pairs.PQ_INPUTS, (fluid == "Water" ? Pwater : pri) * 1000, 0);
            double rho_li = coolprop.rhomass();
            //double rho_li = CoolProp.PropsSI("D", "Q", 0, "P", (fluid == "Water" ? Pwater : pri) * 1000, fluid);
            double mgi   = x_i * mr;
            double mli   = (1 - x_i) * mr;
            double esp_i = 1 / (1 + (1 / x_i - 1) * rho_gi / rho_li);
            double Vgi   = (x_i * mr) / (rho_gi * esp_i * Ar_cs);
            double Vli   = (1 - x_i) * mr / (rho_li * (1 - esp_i) * Ar_cs);

            //初始化出口参数
            double x_o     = x_i;
            double mgo     = mgi;
            double mlo     = mli;
            double rho_go  = rho_gi;
            double rho_lo  = rho_li;
            double esp_o   = esp_i;
            double Vgo_set = Vgi;
            double Vlo     = Vli;

            double rho_avg = rho_gi * x_i + rho_li * (1 - x_i);

            coolprop.update(input_pairs.QT_INPUTS, 0, tsat);
            double ViscosityL = coolprop.viscosity();

            //double ViscosityL = CoolProp.PropsSI("V", "T", tsat, "Q", 0, fluid);
            coolprop.update(input_pairs.QT_INPUTS, 1, tsat);
            double ViscosityV = coolprop.viscosity();
            //double ViscosityV = CoolProp.PropsSI("V", "T", tsat, "Q", 1, fluid);
            double ViscosityTP = x_i * ViscosityV + (1 - x_i) * ViscosityL;
            double ReTP        = g * d_cap / ViscosityTP;
            double f_tpi       = 0.11 * Math.Pow(0.0014 + 68 / ReTP, 0.25);//0.0014表面粗糙度
            double f_tp        = f_tpi;

            double Vgo_cal = 0;
            int    i       = 0;

            double Pro = 0;
            double hro = 0;
            double tro = 0;

            coolprop.update(input_pairs.HmassP_INPUTS, hri * 1000, pri * 1000);
            double tro1 = coolprop.T() - 273.15;
            //double tro1 = CoolProp.PropsSI("T", "H", hri * 1000, "P", pri * 1000, fluid) - 273.15;
            double tro2 = 0;

            if (hri <= h_v && hri >= h_l)
            {
                do
                {
                    if (i != 0)
                    {
                        Vgo_set = Vgo_cal;
                    }
                    //守恒方程
                    double a = f_tp / 4 * Math.Pow(mr, 2) / (2 * rho_avg * Math.Pow(Ar_cs, 2)) * Math.PI * d_cap + mr / lenth_cap * (x_o * Vgo_set + (1 - x_o) * Vlo) - mr / lenth_cap * (x_i * Vgi + (1 - x_i) * Vli);
                    Pro = pri - lenth_cap / Ar_cs * (f_tp / 4 * Math.Pow(mr, 2) / (2 * rho_avg * Math.Pow(Ar_cs, 2)) * Math.PI * d_cap + mr / lenth_cap * (x_o * Vgo_set + (1 - x_o) * Vlo) - mr / lenth_cap * (x_i * Vgi + (1 - x_i) * Vli));
                    hro = 1 / mr * (mr * hri + 1 / 2 * mgi * Math.Pow(Vgi, 2) + 1 / 2 * mli * Math.Pow(Vli, 2) - 1 / 2 * mgo * Math.Pow(Vgo_set, 2) - 1 / 2 * mlo * Math.Pow(Vlo, 2));

                    //新一轮赋值
                    coolprop.update(input_pairs.PQ_INPUTS, Pro * 1000, 0);
                    double tsato = coolprop.T();
                    //double tsato = CoolProp.PropsSI("T", "P", Pro * 1000, "Q", 0, fluid);
                    coolprop.update(input_pairs.QT_INPUTS, 0, tsato);
                    double h_lo = coolprop.hmass();
                    //double h_lo = CoolProp.PropsSI("H", "T", tsato, "Q", 0, fluid) / 1000;
                    coolprop.update(input_pairs.QT_INPUTS, 1, tsato);
                    double h_vo = coolprop.hmass();
                    //double h_vo = CoolProp.PropsSI("H", "T", tsato, "Q", 1, fluid) / 1000;
                    coolprop.update(input_pairs.PQ_INPUTS, (fluid == "Water" ? Pwater : Pro) * 1000, 1);
                    rho_go = coolprop.rhomass();
                    //rho_go = CoolProp.PropsSI("D", "Q", 1, "P", (fluid == "Water" ? Pwater : Pro) * 1000, fluid);
                    coolprop.update(input_pairs.PQ_INPUTS, (fluid == "Water" ? Pwater : Pro) * 1000, 0);
                    rho_lo = coolprop.rhomass();
                    //rho_lo = CoolProp.PropsSI("D", "Q", 0, "P", (fluid == "Water" ? Pwater : Pro) * 1000, fluid);
                    x_o     = (hro - h_lo) / (h_vo - h_lo);
                    esp_o   = 1 / (1 + (1 / x_o - 1) * rho_go / rho_lo);
                    Vgo_cal = (x_o * mr) / (rho_go * esp_o * Ar_cs);
                    Vlo     = (1 - x_o) * mr / (rho_lo * (1 - esp_o) * Ar_cs);
                    mgo     = x_o * mr;
                    mlo     = (1 - x_o) * mr;
                    rho_avg = (rho_gi * x_i + rho_li * (1 - x_i) + rho_go * x_o + rho_lo * (1 - x_o)) / 2;

                    coolprop.update(input_pairs.QT_INPUTS, 0, tsato);
                    double ViscosityLo = coolprop.viscosity();
                    //double ViscosityLo = CoolProp.PropsSI("V", "T", tsato, "Q", 0, fluid);
                    coolprop.update(input_pairs.QT_INPUTS, 1, tsato);
                    double ViscosityVo = coolprop.viscosity();
                    //double ViscosityVo = CoolProp.PropsSI("V", "T", tsato, "Q", 1, fluid);
                    double ViscosityTPo = x_o * ViscosityVo + (1 - x_o) * ViscosityLo;
                    double ReTPo        = g * d_cap / ViscosityTPo;
                    double f_tpo        = 0.11 * Math.Pow(0.0014 + 68 / ReTPo, 0.25);
                    f_tp = (f_tpi + f_tpo) / 2;

                    i++;
                } while (Math.Abs((Vgo_cal - Vgo_set) / Vgo_cal) > 0.02);
            }

            else
            {
                do
                {
                    if (i != 0)
                    {
                        tro1 = tro2;
                    }
                    if (i != 0)
                    {
                        Vgo_set = Vgo_cal;
                    }
                    //守恒方程
                    double a = f_tp / 4 * Math.Pow(mr, 2) / (2 * rho_avg * Math.Pow(Ar_cs, 2)) * Math.PI * d_cap + mr / lenth_cap * (x_o * Vgo_set + (1 - x_o) * Vlo) - mr / lenth_cap * (x_i * Vgi + (1 - x_i) * Vli);
                    Pro = pri - lenth_cap / Ar_cs * (f_tp / 4 * Math.Pow(mr, 2) / (2 * rho_avg * Math.Pow(Ar_cs, 2)) * Math.PI * d_cap + mr / lenth_cap * (x_o * Vgo_set + (1 - x_o) * Vlo) - mr / lenth_cap * (x_i * Vgi + (1 - x_i) * Vli));
                    hro = 1 / mr * (mr * hri + 1 / 2 * mgi * Math.Pow(Vgi, 2) + 1 / 2 * mli * Math.Pow(Vli, 2) - 1 / 2 * mgo * Math.Pow(Vgo_set, 2) - 1 / 2 * mlo * Math.Pow(Vlo, 2));

                    //新一轮赋值
                    coolprop.update(input_pairs.PQ_INPUTS, Pro * 1000, 0);
                    double tsato = coolprop.T();
                    //double tsato = CoolProp.PropsSI("T", "P", Pro * 1000, "Q", 0, fluid);
                    coolprop.update(input_pairs.QT_INPUTS, 0, tsato);
                    double h_lo = coolprop.hmass();
                    //double h_lo = CoolProp.PropsSI("H", "T", tsato, "Q", 0, fluid) / 1000;
                    coolprop.update(input_pairs.QT_INPUTS, 1, tsato);
                    double h_vo = coolprop.hmass();
                    //double h_vo = CoolProp.PropsSI("H", "T", tsato, "Q", 1, fluid) / 1000;
                    coolprop.update(input_pairs.PQ_INPUTS, (fluid == "Water" ? Pwater : Pro) * 1000, 1);
                    rho_go = coolprop.rhomass();
                    //rho_go = CoolProp.PropsSI("D", "Q", 1, "P", (fluid == "Water" ? Pwater : Pro) * 1000, fluid);
                    coolprop.update(input_pairs.PQ_INPUTS, (fluid == "Water" ? Pwater : Pro) * 1000, 0);
                    rho_lo = coolprop.rhomass();
                    //rho_lo = CoolProp.PropsSI("D", "Q", 0, "P", (fluid == "Water" ? Pwater : Pro) * 1000, fluid);

                    x_o     = (hro - h_lo) / (h_vo - h_lo);
                    esp_o   = 1 / (1 + (1 / x_o - 1) * rho_go / rho_lo);
                    Vgo_cal = (x_o * mr) / (rho_go * esp_o * Ar_cs);
                    Vlo     = (1 - x_o) * mr / (rho_lo * (1 - esp_o) * Ar_cs);
                    mgo     = x_o * mr;
                    mlo     = (1 - x_o) * mr;
                    rho_avg = (rho_gi * x_i + rho_li * (1 - x_i) + rho_go * x_o + rho_lo * (1 - x_o)) / 2;

                    coolprop.update(input_pairs.QT_INPUTS, 0, tsato);
                    double ViscosityLo = coolprop.viscosity();
                    //double ViscosityLo = CoolProp.PropsSI("V", "T", tsato, "Q", 0, fluid);
                    coolprop.update(input_pairs.QT_INPUTS, 1, tsato);
                    double ViscosityVo = coolprop.viscosity();
                    //double ViscosityVo = CoolProp.PropsSI("V", "T", tsato, "Q", 1, fluid);
                    double ViscosityTPo = x_o * ViscosityVo + (1 - x_o) * ViscosityLo;
                    double ReTPo        = g * d_cap / ViscosityTPo;
                    double f_tpo        = 0.11 * Math.Pow(0.0014 + 68 / ReTPo, 0.25);
                    f_tp = (f_tpi + f_tpo) / 2;
                    coolprop.update(input_pairs.HmassP_INPUTS, hro * 1000, Pro * 1000);
                    tro2 = coolprop.T() - 273.15;
                    //tro2 = CoolProp.PropsSI("T", "H", hro * 1000, "P", Pro * 1000, fluid) - 273.15;

                    i++;
                } while (Math.Abs(tro2 - tro1) > 0.02);
            }

            double DP_cap = pri - Pro;

            coolprop.update(input_pairs.HmassP_INPUTS, hro * 1000, Pro * 1000);
            tro = coolprop.T() - 273.15;
            //tro = CoolProp.PropsSI("T", "H", hro * 1000, "P", Pro * 1000, fluid) - 273.15;

            res_cap.pro    = Pro;
            res_cap.hro    = hro;
            res_cap.tro    = tro;
            res_cap.DP_cap = DP_cap;
            res_cap.x_o    = x_o;

            return(res_cap);
        }
예제 #2
0
        public static CalcResult CircuitCalc(int index, CirArr[] cirArr, CircuitNumber CircuitInfo, int Nrow, int[] Ntube, int Nelement, string fluid,
                                             double l, Geometry geo, double[, ,] ta, double[, ,] RH, double tri, double pri, double hri, double mr, double[,] ma, double[,] ha, double[,] haw,
                                             double eta_surface, double zh, double zdp, int hexType, double thickness, double conductivity, double Pwater, CapiliaryInput cap_inlet, CapiliaryInput cap_outlet, AbstractState coolprop, double[,] SourceTableData)
        {
            #region 算进口毛细管
            //调用毛细管守恒方程模型
            ///
            double          DP_cap     = 0;
            int             N          = 1;
            Capiliary_res[] res_cap_in = new Capiliary_res[N];
            if (cap_inlet.d_cap[index] == 0 && cap_inlet.lenth_cap[index] == 0)
            {
                pri = pri;
                hri = hri;
                tri = tri;
            }
            else
            {
                for (int i = 0; i < N; i++)
                {
                    res_cap_in[i] = Capiliary.CapiliaryCalc(index, fluid, cap_inlet.d_cap[index], cap_inlet.lenth_cap[index] / N, tri, pri, hri, mr, Pwater, hexType, coolprop, SourceTableData);
                    pri           = res_cap_in[i].pro;
                    hri           = res_cap_in[i].hro;
                    tri           = res_cap_in[i].tro;
                    DP_cap       += res_cap_in[i].DP_cap;
                }
            }
            #endregion

            #region 算流路
            ///
            //******蒸发器毛细管******//

            int N_tube = Ntube[0];
            //int Ncir = CircuitInfo.number[0];
            int          Ncir      = CircuitInfo.TubeofCir.Length;
            int[]        TubeofCir = CircuitInfo.TubeofCir;
            CalcResult   res_cir   = new CalcResult();
            CalcResult[] r         = new CalcResult[TubeofCir[index]];

            int iRow  = 0;
            int iTube = 0;

            double[] tai = new double[Nelement];
            double[] RHi = new double[Nelement];
            double[, ,] taout_calc  = new double[Nelement, N_tube, Nrow];
            double[, ,] RHout_calc  = new double[Nelement, N_tube, Nrow];
            double[,] Q_detail      = new double[N_tube, Nrow];//detail output
            double[,] DP_detail     = new double[N_tube, Nrow];
            double[,] Tri_detail    = new double[N_tube, Nrow];
            double[,] Pri_detail    = new double[N_tube, Nrow];
            double[,] hri_detail    = new double[N_tube, Nrow];
            double[,] Tro_detail    = new double[N_tube, Nrow];
            double[,] Pro_detail    = new double[N_tube, Nrow];
            double[,] hro_detail    = new double[N_tube, Nrow];//
            double[,] href_detail   = new double[N_tube, Nrow];
            double[,] mr_detail     = new double[N_tube, Nrow];
            double[,] charge_detail = new double[N_tube, Nrow];
            double   Ar       = 0;
            double   Aa       = 0;
            double   Aa_tube  = 0;
            double   Aa_fin   = 0;
            double   Ar_cs    = 0;
            double   pri_tube = 0;
            double   tri_tube = 0;
            double   hri_tube = 0;
            double[] ma_tube  = new double[Nelement];
            double[] ha_tube  = new double[Nelement];
            double[] haw_tube = new double[Nelement];
            int      index2   = 0;

            CheckAir airConverge = new CheckAir();
            int      iter        = 0;
            //ma = ma / (N_tube*Nelement); //air flow distribution to be considered

            if (index == 0)
            {
                index2 = 0;
            }
            else
            {
                for (int i = 1; i <= index; i++)
                {
                    index2 += TubeofCir[i - 1];
                }
            }
            //do
            //{
            pri_tube   = pri;
            tri_tube   = tri;
            hri_tube   = hri;
            res_cir.DP = 0;
            // res_cir.Tao += r.Tao;
            res_cir.Q     = 0;
            res_cir.M     = 0;
            res_cir.Tro   = 0;
            res_cir.Pro   = 0;
            res_cir.hro   = 0;
            res_cir.x_o   = 0;
            res_cir.Vel_r = 0;
            res_cir.href  = 0;
            res_cir.R_1   = 0;
            res_cir.R_1a  = 0;
            res_cir.R_1r  = 0;
            res_cir.mr    = 0;
            for (int i = 0; i < TubeofCir[index]; i++)     //to be updated //Nrow * N_tube
            {
                //index2 = index == 1 ? 0 : (index - 1) * TubeofCir[index - 1 - 1];
                iRow  = cirArr[i + index2].iRow;
                iTube = cirArr[i + index2].iTube;

                Ar      = geo.ElementArea[iTube, iRow].A_r;
                Aa      = geo.ElementArea[iTube, iRow].A_a;
                Aa_tube = geo.ElementArea[iTube, iRow].Aa_tube;
                Aa_fin  = geo.ElementArea[iTube, iRow].Aa_fin;
                Ar_cs   = geo.ElementArea[iTube, iRow].A_r_cs;
                //tai=ta[,iTube,iRow];
                for (int j = 0; j < Nelement; j++)
                {
                    tai[j]      = ta[j, iTube, iRow];
                    RHi[j]      = RH[j, iTube, iRow];
                    ma_tube[j]  = ma[iTube, j];
                    ha_tube[j]  = ha[iTube, j];
                    haw_tube[j] = haw[iTube, j];
                }

                r[i] = Tube.TubeCalc(Nelement, fluid, l, Aa_fin, Aa_tube, Ar_cs, Ar, geo, tai, RHi, tri_tube, pri_tube, hri_tube,
                                     mr, ma_tube, ha_tube, haw_tube, eta_surface, zh, zdp, hexType, thickness, conductivity, Pwater, coolprop, SourceTableData);
                if (r[i].Pro < 0)
                {
                    res_cir.Pro = -10000000; return(res_cir);
                }

                /*if (Airdirection == "顺流")
                 * {
                 *  for (int j = 0; j < Nelement; j++)
                 *  {
                 *      taout_calc[j, iTube, iRow] = r[i].Tao;
                 *      RHout_calc[j, iTube, iRow] = r[i].RHout;
                 *      ta[j, iTube, iRow+1] = r[i].Tao;
                 *      RH[j, iTube, iRow+1] = r[i].RHout;
                 *  }
                 * }
                 * else//Counter
                 * {
                 *  for(int j=0;j<Nelement;j++)
                 *  {
                 *      taout_calc[j, iTube, iRow] =r[i].Tao_Detail[0, 0, j];
                 *      RHout_calc[j, iTube, iRow] = r[i].RHout;
                 *  }
                 * }*/

                for (int j = 0; j < Nelement; j++)
                {
                    taout_calc[j, iTube, iRow] = r[i].Tao_Detail[0, 0, j];
                    RHout_calc[j, iTube, iRow] = r[i].RHout;
                }



                Tri_detail[iTube, iRow] = tri_tube;
                Pri_detail[iTube, iRow] = pri_tube;
                hri_detail[iTube, iRow] = hri_tube;
                tri_tube    = r[i].Tro;
                pri_tube    = r[i].Pro;
                hri_tube    = r[i].hro;
                res_cir.DP += r[i].DP;
                // res_cir.Tao += r.Tao;
                res_cir.Q             += r[i].Q;
                Q_detail[iTube, iRow]  = r[i].Q;   //detail output
                DP_detail[iTube, iRow] = r[i].DP;

                Tro_detail[iTube, iRow]    = r[i].Tro;
                Pro_detail[iTube, iRow]    = r[i].Pro;
                hro_detail[iTube, iRow]    = r[i].hro;
                href_detail[iTube, iRow]   = r[i].href;
                mr_detail[iTube, iRow]     = mr;
                charge_detail[iTube, iRow] = r[i].M;
                res_cir.M    += r[i].M;
                res_cir.Tro   = r[i].Tro;
                res_cir.Pro   = r[i].Pro;
                res_cir.hro   = r[i].hro;
                res_cir.x_o   = r[i].x_o;
                res_cir.Vel_r = r[i].Vel_r;
                res_cir.href += r[i].href;
                res_cir.R_1  += r[i].R_1;
                res_cir.R_1a += r[i].R_1a;
                res_cir.R_1r += r[i].R_1r;
                res_cir.Tri   = r[i].Tri;
                res_cir.x_i   = r[i].x_i;
            }

            /*
             *  if (Airdirection == "顺流")
             *      airConverge.flag = true;
             *  else//Counter
             *  {
             *      airConverge = CheckAirConvergeforCircuits.CheckAirConverge(Nrow, N_tube, Nelement, ta, RH, taout_calc, RHout_calc);
             *      ta = airConverge.ta;
             *      RH = airConverge.RH;
             *      iter++;
             *  }
             * } while (!airConverge.flag && iter < 100);
             */

            //if (iter >= 100)
            //{
            //    throw new Exception("iter for AirConverge > 100.");
            //}
            res_cir.mr         = mr;
            res_cir.Tao_Detail = taout_calc;
            res_cir.RHo_Detail = RHout_calc;

            //res_cir.Tao = res_cir.Tao / Nelement;
            res_cir.href        = res_cir.href / TubeofCir[index];
            res_cir.R_1         = res_cir.R_1 / TubeofCir[index];
            res_cir.R_1a        = res_cir.R_1a / TubeofCir[index];
            res_cir.R_1r        = res_cir.R_1r / TubeofCir[index];
            res_cir.Q_detail    = Q_detail;//detail output
            res_cir.DP_detail   = DP_detail;
            res_cir.Tri_detail  = Tri_detail;
            res_cir.Pri_detail  = Pri_detail;
            res_cir.hri_detail  = hri_detail;
            res_cir.Tro_detail  = Tro_detail;
            res_cir.Pro_detail  = Pro_detail;
            res_cir.hro_detail  = hro_detail;
            res_cir.href_detail = href_detail;
            res_cir.mr_detail   = mr_detail;

            #endregion

            #region 算出口毛细管
            //调用毛细管守恒方程模型  ----需要校核,调整----
            ///
            N = 1;
            Capiliary_res[] res_cap_out = new Capiliary_res[N];
            //double DP_cap = 0;
            if (cap_outlet.d_cap[index] == 0 && cap_outlet.lenth_cap[index] == 0)
            {
                pri = pri;
                hri = hri;
                tri = tri;
            }
            else
            {
                for (int i = 0; i < N; i++)
                {
                    res_cap_out[i] = Capiliary.CapiliaryCalc(index, fluid, cap_outlet.d_cap[index], cap_outlet.lenth_cap[index] / N, res_cir.Tro, res_cir.Pro, res_cir.hro, mr, Pwater, hexType, coolprop, SourceTableData);
                    res_cir.Pro    = res_cap_out[i].pro;
                    res_cir.hro    = res_cap_out[i].hro;
                    res_cir.Tro    = res_cap_out[i].tro;
                    DP_cap        += res_cap_out[i].DP_cap;
                }
            }
            #endregion

            //增加毛细管模型的单流路总压降
            res_cir.DP     = res_cir.DP + DP_cap;
            res_cir.DP_cap = DP_cap;


            res_cir.charge_detail = charge_detail;

            return(res_cir);
        }