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3e93bb69a1
* [coolprop] Cleanup * Fix uwp * [refprop-headers] Update * [if97] Avoid encoding warnings * [msgpack] More boost dependencies Cf. https://github.com/msgpack/msgpack-c/wiki/install_boost * [coolprop] Use msgpack endianess --------- Co-authored-by: Cheney-Wang <850426846@qq.com>
49 lines
3.0 KiB
Diff
49 lines
3.0 KiB
Diff
diff --git a/IF97.h b/IF97.h
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index 864f3a0..4e6cab5 100644
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--- a/IF97.h
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+++ b/IF97.h
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@@ -52,7 +52,7 @@ namespace IF97
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// IF97 Constants
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const double Tcrit = 647.096; // K
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const double Pcrit = 22.064*p_fact; // MPa*
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- const double Rhocrit = 322.0; // kg/m³
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+ const double Rhocrit = 322.0; // kg/m^3
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const double Scrit = 4.41202148223476*R_fact; // kJ*/kg-K (needed for backward eqn. in Region 3(a)(b)
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const double Ttrip = 273.16; // K
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const double Ptrip = 0.000611656*p_fact; // MPa*
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@@ -2394,7 +2394,7 @@ namespace IF97
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// The equation is rearranged to solve for rho and turned
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// into functions f(T,P,rho0) and f'(T,P,rho0) for the
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// Newton-Raphson technique. Functions for
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- // dphi/ddelta and d²phi/ddelta² were also required. These
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+ // dphi/ddelta and d^2phi/ddelta^2 were also required. These
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// additional Taylor functions are defined above.
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//
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double f(double T, double p, double rho0) const{
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@@ -4172,7 +4172,7 @@ namespace IF97
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return RegionOutput( IF97_HMASS,RegionOutputBackward(Pmax,s,IF97_SMASS),Pmax, NONE);
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else {
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// Determining H(s) along Tmax is difficult because there is no direct p(T,s) formulation.
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- // This linear combination fit h(s)=a*ln(s)+b/s+c/s²+d is not perfect, but it's close
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+ // This linear combination fit h(s)=a*ln(s)+b/s+c/s^2+d is not perfect, but it's close
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// and can serve as a limit along that Tmax boundary. Coefficients in HTmaxdata above.
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// There is a better way to do this using Newton-Raphson on Tmax = T(p,s), but it is iterative and slow.
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double ETA = Hmax_n[0]*log(sigma) + Hmax_n[1]/sigma + Hmax_n[2]/pow(sigma,2) +Hmax_n[3];
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@@ -4323,14 +4323,14 @@ namespace IF97
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inline double cvmass_Tp(double T, double p){ return RegionOutput( IF97_CVMASS, T, p, NONE); };
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/// Get the speed of sound [m/s] as a function of T [K] and p [Pa]
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inline double speed_sound_Tp(double T, double p){ return RegionOutput( IF97_W, T, p, NONE); };
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- /// Get the [d(rho)/d(p)]T [kg/m³/Pa] as a function of T [K] and p [Pa]
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+ /// Get the [d(rho)/d(p)]T [kg/m^3/Pa] as a function of T [K] and p [Pa]
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inline double drhodp_Tp(double T, double p){ return RegionOutput( IF97_DRHODP, T, p, NONE); };
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// ******************************************************************************** //
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// Transport Properties //
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// ******************************************************************************** //
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- /// Get the viscosity [Pa-s] as a function of T [K] and Rho [kg/m³]
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+ /// Get the viscosity [Pa-s] as a function of T [K] and Rho [kg/m^3]
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inline double visc_TRho(double T, double rho) {
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// Since we have density, we don't need to determine the region for viscosity.
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static Region1 R1; // All regions use base region equations for visc(T,rho).
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