ruoyi-api/ruoyi-ngtools/src/main/java/com/ruoyi/ngCalTools/service/ThermService.java

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2025-02-04 09:20:17 +00:00
package com.ruoyi.ngCalTools.service;
import com.ruoyi.ngCalTools.model.GasProps;
import com.ruoyi.ngCalTools.utils.GasConstants;
import org.springframework.stereotype.Service;
@Service
public class ThermService {
private static final double CAL_TH = 4.1840;
public int coefA = 0;
public int coefB = 1;
public int coefC = 2;
public int coefD = 3;
public int coefE = 4;
public int coefF = 5;
public int coefG = 6;
public int coefH = 7;
public int coefI = 8;
public int coefJ = 9;
public int coefK = 10;
double dPdD;// partial deriv of P wrt D
double dPdT;// partial deriv of P wrt T
double dSi;// ideal gas specific entropy, kJ/kg.K
double dTold;// temperature previously used
double dMrxold;// mixture molar mass previously used
//set the number of points for quadrature
int GK_points = 5;
// 初始化 GK_root 数组
double[] GK_root = { 0.14887433898163121088, 0.43339539412924719080, 0.67940956829902440263, 0.86506336668898451073, 0.97390652851717172008 };
// 初始化 GK_weight 数组
double[] GK_weight = { 0.29552422471475286217, 0.26926671930999634918, 0.21908636251598204295, 0.14945134915058059038, 0.066671344308688137179 };
private final double[][] ThermConstants = {
{-29776.4, 7.95454, 43.9417, 1037.09, 1.56373, 813.205, -24.9027, 1019.98, -10.1601, 1070.14, -20.0615},
{-3495.34, 6.95587, 0.272892, 662.738, -0.291318, -680.562, 1.78980, 1740.06, 0.0, 100.0, 4.49823},
{20.7307, 6.96237, 2.68645, 500.371, -2.56429, -530.443, 3.91921, 500.198, 2.13290, 2197.22, 5.81381},
{-37524.4, 7.98139, 24.3668, 752.320, 3.53990, 272.846, 8.44724, 1020.13, -13.2732, 869.510, -22.4010},
{-56072.1, 8.14319, 37.0629, 735.402, 9.38159, 247.190, 13.4556, 1454.78, -11.7342, 984.518, -24.0426},
{-13773.1, 7.97183, 6.27078, 2572.63, 2.05010, 1156.72, 0.0, 100.0, 0.0, 100.0, -3.24989},
{-10085.4, 7.94680, -0.08380, 433.801, 2.85539, 843.792, 6.31595, 1481.43, -2.88457, 1102.23, -0.51551},
{-5565.60, 6.66789, 2.33458, 2584.98, 0.749019, 559.656, 0.0, 100.0, 0.0, 100.0, -7.94821},
{-2753.49, 6.95854, 2.02441, 1541.22, 0.096774, 3674.81, 0.0, 100.0, 0.0, 100.0, 6.23387},
{-3497.45, 6.96302, 2.40013, 2522.05, 2.21752, 1154.15, 0.0, 100.0, 0.0, 100.0, 9.19749},
{-72387.0, 17.8143, 58.2062, 1787.39, 40.7621, 808.645, 0.0, 100.0, 0.0, 100.0, -44.1341},
{-72674.8, 18.6383, 57.4178, 1792.73, 38.6599, 814.151, 0.0, 100.0, 0.0, 100.0, -46.1938},
{-91505.5, 21.3861, 74.3410, 1701.58, 47.0587, 775.899, 0.0, 100.0, 0.0, 100.0, -60.2474},
{-83845.2, 22.5012, 69.5789, 1719.58, 46.2164, 802.174, 0.0, 100.0, 0.0, 100.0, -62.2197},
{-94982.5, 26.6225, 80.3819, 1718.49, 55.6598, 802.069, 0.0, 100.0, 0.0, 100.0, -77.5366},
{-103353.0, 30.4029, 90.6941, 1669.32, 63.2028, 786.001, 0.0, 100.0, 0.0, 100.0, -92.0164},
{-109674.0, 34.0847, 100.253, 1611.55, 69.7675, 768.847, 0.0, 100.0, 0.0, 100.0, -106.149},
{-122599.0, 38.5014, 111.446, 1646.48, 80.5015, 781.588, 0.0, 100.0, 0.0, 100.0, -122.444},
{-133564.0, 42.7143, 122.173, 1654.85, 90.2255, 785.564, 0.0, 100.0, 0.0, 100.0, -138.006},
{0.0, 4.9680, 0.0, 100.0, 0.0, 100.0, 0.0, 100.0, 0.0, 100.0, 0.0},
{0.0, 4.9680, 0.0, 100.0, 0.0, 100.0, 0.0, 100.0, 0.0, 100.0, 0.0}
};
public void calculateThermodynamicProperties(GasProps gasProps) {
// 实现热力学计算逻辑
double cp = calculateCpiMolar(gasProps);
gasProps.setDCpi(cp * 1000 / gasProps.getDMrx());
// 其他计算...
}
public void Run(GasProps gasProps, DetailService detailService)
{
//local variables
double c, x, y, z;
//first run basic set of functions within AGA 8 (1994) Detail Method
detailService.run(gasProps);
//find first partial derivative of Z wrt D
detailService.dZdD(gasProps.dDf);
//find real gas cv, cp, specific enthalpy and entropy
CprCvrHS(gasProps, detailService);
//ratio of real gas specific heats
gasProps.dk = gasProps.dCp / gasProps.dCv;
//solve c in three steps, for clarity and ease of debugging
x = gasProps.dk * GasConstants.RGAS * 1000.0 * gasProps.dTf;
y = gasProps.dMrx;
z = gasProps.dZf + gasProps.dDf * detailService.ddZdD;
//calculate c, which is SOS^2
c = (x / y) * z;
//speed of sound
gasProps.dSOS = Math.sqrt(c);
//calculate the real gas isentropic exponent
//using expression functionally equivalent to Equation 3.2
gasProps.dKappa = (c * gasProps.dRhof) / gasProps.dPf;
return;
}
private double calculateCpiMolar(GasProps gasProps) {
double cp = 0.0;
double Cpx;
double DT, FT, HT, JT;
double Dx, Fx, Hx, Jx;
double T;
T = gasProps.dTf;
for (int i = 0; i < GasConstants.NUMBEROFCOMPONENTS; i++) {
if (gasProps.getAdMixture()[i] > 0) {
// 计算每个组分的贡献
Cpx = 0.0;
// calculate species intermediate terms
DT = ThermConstants[i][ coefD] / T;
FT = ThermConstants[i][ coefF] / T;
HT = ThermConstants[i][ coefH] / T;
JT = ThermConstants[i][ coefJ] / T;
// use intermediate terms to avoid redundant calcs
Dx = DT / Math.sinh(DT);
Fx = FT / Math.cosh(FT);
Hx = HT / Math.sinh(HT);
Jx = JT / Math.cosh(JT);
Cpx += ThermConstants[i][ coefB];
Cpx += ThermConstants[i][ coefC] * Dx * Dx;
Cpx += ThermConstants[i][ coefE] * Fx * Fx;
Cpx += ThermConstants[i][ coefG] * Hx * Hx;
Cpx += ThermConstants[i][ coefI] * Jx * Jx;
//use current mole fraction to weight the contribution
Cpx *= gasProps.adMixture[i];
//add this contribution to the sum
cp += Cpx;
}
}
return cp * CAL_TH;
}
// coth 函数实现
private static double coth(double x) {
return 1.0 / Math.tanh(x);
}
// Ho 函数
public double Ho(GasProps gasProps) {
double H = 0.0;
double Hx;
double DT, FT, HT, JT;
double cothDT, tanhFT, cothHT, tanhJT;
double T = gasProps.dTf;
for (int i = 0; i < GasConstants.NUMBEROFCOMPONENTS; i++) {
if (gasProps.adMixture[i] <= 0.0) continue;
Hx = 0.0;
DT = ThermConstants[i][coefD] / T;
FT = ThermConstants[i][coefF] / T;
HT = ThermConstants[i][coefH] / T;
JT = ThermConstants[i][coefJ] / T;
cothDT = coth(DT);
tanhFT = Math.tanh(FT);
cothHT = coth(HT);
tanhJT = Math.tanh(JT);
Hx += ThermConstants[i][coefA];
Hx += ThermConstants[i][coefB] * T;
Hx += ThermConstants[i][coefC] * ThermConstants[i][coefD] * cothDT;
Hx -= ThermConstants[i][coefE] * ThermConstants[i][coefF] * tanhFT;
Hx += ThermConstants[i][coefG] * ThermConstants[i][coefH] * cothHT;
Hx -= ThermConstants[i][coefI] * ThermConstants[i][coefJ] * tanhJT;
Hx *= gasProps.adMixture[i];
H += Hx;
}
H *= CAL_TH;
H /= gasProps.dMrx;
return H * 1000.0;
}
// So 函数
public double So(GasProps gasProps) {
double S = 0.0;
double Sx;
double DT, FT, HT, JT;
double cothDT, tanhFT, cothHT, tanhJT;
double sinhDT, coshFT, sinhHT, coshJT;
double T = gasProps.dTf;
for (int i = 0; i < GasConstants.NUMBEROFCOMPONENTS; i++) {
if (gasProps.adMixture[i] <= 0.0) continue;
Sx = 0.0;
DT = ThermConstants[i][coefD] / T;
FT = ThermConstants[i][coefF] / T;
HT = ThermConstants[i][coefH] / T;
JT = ThermConstants[i][coefJ] / T;
cothDT = coth(DT);
tanhFT = Math.tanh(FT);
cothHT = coth(HT);
tanhJT = Math.tanh(JT);
sinhDT = Math.sinh(DT);
coshFT = Math.cosh(FT);
sinhHT = Math.sinh(HT);
coshJT = Math.cosh(JT);
Sx += ThermConstants[i][coefK];
Sx += ThermConstants[i][coefB] * Math.log(T);
Sx += ThermConstants[i][coefC] * (DT * cothDT - Math.log(sinhDT));
Sx -= ThermConstants[i][coefE] * (FT * tanhFT - Math.log(coshFT));
Sx += ThermConstants[i][coefG] * (HT * cothHT - Math.log(sinhHT));
Sx -= ThermConstants[i][coefI] * (JT * tanhJT - Math.log(coshJT));
Sx *= gasProps.adMixture[i];
S += Sx;
}
S *= CAL_TH;
S /= gasProps.dMrx;
return S * 1000.0;
}
// CprCvrHS 函数
public void CprCvrHS(GasProps gasProps, DetailService detailService) {
double Cvinc = 0.0;
double Cvr, Cpr;
double Hinc = 0.0;
double Sinc = 0.0;
double Smixing = 0.0;
double Cp = calculateCpiMolar(gasProps);
double Si;
gasProps.dHo = Ho(gasProps);
Si = So(gasProps);
gasProps.dCpi = (Cp * 1000.0) / gasProps.dMrx;
for (int i = 0; i < GK_points; i++) {
double x = gasProps.dDf * (1.0 + GK_root[i]) / 2.0;
detailService.zdetail(x);
detailService.dZdT(x);
detailService.d2ZdT2(x);
Hinc += GK_weight[i] * detailService.ddZdT / x;
Cvinc += GK_weight[i] * (2.0 * detailService.ddZdT + gasProps.dTf * detailService.dd2ZdT2) / x;
Sinc += GK_weight[i] * (detailService.dZ + gasProps.dTf * detailService.ddZdT - 1.0) / x;
x = gasProps.dDf * (1.0 - GK_root[i]) / 2.0;
detailService.zdetail(x);
detailService.dZdT(x);
detailService.d2ZdT2(x);
Hinc += GK_weight[i] * detailService.ddZdT / x;
Cvinc += GK_weight[i] * (2.0 * detailService.ddZdT + gasProps.dTf * detailService.dd2ZdT2) / x;
Sinc += GK_weight[i] * (detailService.dZ + gasProps.dTf * detailService.ddZdT - 1.0) / x;
}
detailService.zdetail(gasProps.dDf);
detailService.dZdT(gasProps.dDf);
detailService.d2ZdT2(gasProps.dDf);
Cvr = Cp - GasConstants.RGAS * (1.0 + gasProps.dTf * Cvinc * 0.5 * gasProps.dDf);
double a = (gasProps.dZf + gasProps.dTf * detailService.ddZdT);
double b = (gasProps.dZf + gasProps.dDf * detailService.ddZdD);
double dPdT =GasConstants. RGAS * gasProps.dDf * a;
double dPdD = GasConstants.RGAS * gasProps.dTf * b;
Cpr = Cvr + GasConstants.RGAS * ((a * a) / b);
Cpr /= gasProps.dMrx;
Cvr /= gasProps.dMrx;
gasProps.dCv = Cvr * 1000.0;
gasProps.dCp = Cpr * 1000.0;
gasProps.dH = gasProps.dHo + 1000.0 * GasConstants.RGAS * gasProps.dTf * (gasProps.dZf - 1.0 - gasProps.dTf * Hinc * 0.5 * gasProps.dDf) / gasProps.dMrx;
for (int i = 0; i < GasConstants.NUMBEROFCOMPONENTS; i++) {
if (gasProps.adMixture[i] != 0) Smixing += gasProps.adMixture[i] * Math.log(gasProps.adMixture[i]);
}
Smixing *= GasConstants.RGAS;
gasProps.dS = Si - Smixing - 1000.0 * GasConstants.RGAS * (Math.log(gasProps.dPf / 101325.0) - Math.log(gasProps.dZf) + Sinc * 0.5 * gasProps.dDf) / gasProps.dMrx;
}
// HS_Mode 函数
public void HS_Mode( GasProps gasProps, DetailService detailService, double H, double S, boolean bGuess) {
double s0 = S;
double h0 = H;
double t1, t2, tmin, tmax;
double p1, p2, px, pmin, pmax;
double delta1, delta2;
double tolerance = 0.001;
if (bGuess) {
t1 = gasProps.dTf;
px = gasProps.dPf;
pmax = px * 2.0;
pmin = px * 0.1;
tmax = t1 * 1.5;
tmin = t1 * 0.67;
} else {
t1 = 273.15;
px = 1013250.0;
pmax = GasConstants.P_MAX;
pmin = 10000.0;
tmax = GasConstants.T_MAX;
tmin = GasConstants.T_MIN;
}
t2 = t1 + 10.0;
detailService.run(gasProps);
double h1 = H(gasProps, detailService) - h0;
for (int i = 0; i < GasConstants.MAX_NUM_OF_ITERATIONS; i++) {
gasProps.dTf = t2;
p1 = px;
p2 = px * 0.1;
gasProps.dPf = p1;
detailService.run(gasProps);
double s1 = S(gasProps, detailService) - s0;
for (int j = 0; j < GasConstants.MAX_NUM_OF_ITERATIONS; j++) {
gasProps.dPf = p2;
detailService.run(gasProps);
double s2 = S(gasProps, detailService) - s0;
delta2 = Math.abs(s1 - s2) / s0;
if (delta2 < tolerance) break;
double p0 = p2;
p2 = (p1 * s2 - p2 * s1) / (s2 - s1);
if (p2 <= pmin) p2 = pmin;
if (p2 >= pmax) p2 = pmax;
p1 = p0;
s1 = s2;
}
if (gasProps.lStatus == GasConstants.MAX_NUM_OF_ITERATIONS_EXCEEDED) break;
double h2 = H(gasProps, detailService) - h0;
delta1 = Math.abs(h1 - h2) / h0;
if (delta1 < tolerance && i > 0) break;
double t0 = t2;
t2 = (t1 * h2 - t2 * h1) / (h2 - h1);
if (t2 >= tmax) t2 = tmax;
if (t2 <= tmin) {
t2 = t0 + 10.0;
gasProps.dTf = t2;
detailService.run(gasProps);
h2 = H(gasProps, detailService) - h0;
}
t1 = t0;
h1 = h2;
}
if (gasProps.lStatus == GasConstants.MAX_NUM_OF_ITERATIONS_EXCEEDED) {
gasProps.lStatus = GasConstants.MAX_NUM_OF_ITERATIONS_EXCEEDED;
}
}
// H 函数
public double H(GasProps gasProps, DetailService detailService) {
double Hinc = 0.0;
gasProps.dHo = Ho(gasProps);
for (int i = 0; i < GK_points; i++) {
double x = gasProps.dDf * (1.0 + GK_root[i]) / 2.0;
detailService.zdetail(x);
detailService.dZdT(x);
detailService.d2ZdT2(x);
Hinc += GK_weight[i] * detailService.ddZdT / x;
if (i == 10) break;
x = gasProps.dDf * (1.0 - GK_root[i]) / 2.0;
detailService.zdetail(x);
detailService.dZdT(x);
detailService.d2ZdT2(x);
Hinc += GK_weight[i] * detailService.ddZdT / x;
}
detailService.zdetail(gasProps.dDf);
detailService.dZdT(gasProps.dDf);
detailService.d2ZdT2(gasProps.dDf);
gasProps.dH = gasProps.dHo + 1000.0 * GasConstants.RGAS * gasProps.dTf * (gasProps.dZf - 1.0 - gasProps.dTf * Hinc * 0.5 * gasProps.dDf) / gasProps.dMrx;
return gasProps.dH;
}
double S(GasProps gasProps, DetailService detailService)
{
double Sinc; double Smixing; double x;
int i;
//initialize integral
Sinc = 0.0;
//initialize entropy of mixing
Smixing = 0.0;
//integrate partial derivatives from D=0 to D=D, applying Gauss-Kronrod quadrature
for (i = 0; i <GK_points ; i++)
{
//calculate 1st and 2nd partial derivatives of Z wrt T
x = gasProps.dDf * (1.0 + GK_root[i]) / 2.0; detailService.zdetail(x);
detailService.dZdT(x); detailService.d2ZdT2(x);
Sinc += GK_weight[i] * (detailService.dZ + gasProps.dTf * detailService.ddZdT - 1.0) / x;
if (i == 10) break;
x = gasProps.dDf * (1.0 - GK_root[i]) / 2.0; detailService.zdetail(x);
detailService.dZdT(x); detailService.d2ZdT2(x);
Sinc += GK_weight[i] * (detailService.dZ + gasProps.dTf * detailService.ddZdT - 1.0) / x;
}
//reset Z and partial deivatives dZdT and d2ZdT2
detailService.zdetail(gasProps.dDf);
detailService.dZdT(gasProps.dDf);
detailService.d2ZdT2(gasProps.dDf);
//find ideal gas entropy, but only if temperature or composition have changed
if (gasProps.dTf != dTold || gasProps.dMrx != dMrxold)
{
dSi = So(gasProps); dTold = gasProps.dTf; dMrxold = gasProps.dMrx;
}
//calculate entropy of mixing
for (i = 0; i < GasConstants.NUMBEROFCOMPONENTS; i++)
{
if (gasProps.adMixture[i] != 0) Smixing += gasProps.adMixture[i] * Math.log(gasProps.adMixture[i]);
}
Smixing *= GasConstants.RGAS;
// calculate specific entropy
gasProps.dS = dSi - Smixing - 1000.0 * GasConstants.RGAS * (Math.log(gasProps.dPf / 101325.0) - Math.log(gasProps.dZf) + Sinc * 0.5 * gasProps.dDf) / gasProps.dMrx;
return (gasProps.dS);
}
}