RedlichKwongEoS.h

Go to the documentation of this file.

///////////////////////////////////////////////////////////////////////////////
//
// File: RedlichKwongEoS.h
//
// For more information, please see: http://www.nektar.info
//
// The MIT License
//
// Copyright (c) 2006 Division of Applied Mathematics, Brown University (USA),
// Department of Aeronautics, Imperial College London (UK), and Scientific
// Computing and Imaging Institute, University of Utah (USA).
//
// Permission is hereby granted, free of charge, to any person obtaining a
// copy of this software and associated documentation files (the "Software"),
// to deal in the Software without restriction, including without limitation
// the rights to use, copy, modify, merge, publish, distribute, sublicense,
// and/or sell copies of the Software, and to permit persons to whom the
// Software is furnished to do so, subject to the following conditions:
//
// The above copyright notice and this permission notice shall be included
// in all copies or substantial portions of the Software.
//
// THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS
// OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY,
// FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL
// THE AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR OTHER
// LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, ARISING
// FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER
// DEALINGS IN THE SOFTWARE.
//
// Description: Redlich-Kwong equation of state
//
///////////////////////////////////////////////////////////////////////////////
 
#ifndef NEKTAR_SOLVERS_COMPRESSIBLEFLOWSOLVER_MISC_REDLICHKWONGEOS
#define NEKTAR_SOLVERS_COMPRESSIBLEFLOWSOLVER_MISC_REDLICHKWONGEOS
#include "EquationOfState.h"
#include <cmath>
 
#include <LibUtilities/SimdLib/io.hpp>
 
using namespace std;
 
namespace Nektar
{
 
/**
 * @brief Redlich-Kwong equation of state:
 *       p = RT/(1/rho - b) - a/( sqrt(T / Tc) * (1/rho^2 + b/rho)
 *       with a = 0.42748 * (R*Tc)^2 / Pc
 *            b = 0.08664 * (R*Tc) / Pc
 */
class RedlichKwongEoS : public EquationOfState
{
public:
    friend class MemoryManager<RedlichKwongEoS>;
 
    /// Creates an instance of this class
    static EquationOfStateSharedPtr create(
        const LibUtilities::SessionReaderSharedPtr &pSession)
    {
        EquationOfStateSharedPtr p =
            MemoryManager<RedlichKwongEoS>::AllocateSharedPtr(pSession);
        return p;
    }
 
    /// Name of the class
    static std::string className;
 
protected:
    NekDouble m_a;
    NekDouble m_b;
    NekDouble m_Tc;
    NekDouble m_Pc;
 
    NekDouble v_GetTemperature(const NekDouble &rho, const NekDouble &e) final;
 
    vec_t v_GetTemperature(const vec_t &rho, const vec_t &e) final;
 
    NekDouble v_GetPressure(const NekDouble &rho, const NekDouble &e) final;
 
    vec_t v_GetPressure(const vec_t &rho, const vec_t &e) final;
 
    NekDouble v_GetEntropy(const NekDouble &rho, const NekDouble &e) final;
 
    NekDouble v_GetDPDrho_e(const NekDouble &rho, const NekDouble &e) final;
 
    NekDouble v_GetDPDe_rho(const NekDouble &rho, const NekDouble &e) final;
 
    NekDouble v_GetEFromRhoP(const NekDouble &rho, const NekDouble &p) final;
 
    NekDouble v_GetRhoFromPT(const NekDouble &rho, const NekDouble &p) final;
 
private:
    RedlichKwongEoS(const LibUtilities::SessionReaderSharedPtr &pSession);
 
    ~RedlichKwongEoS(void) override{};
 
    // Alpha term of Redlich-Kwong EoS ( 1.0/sqrt(Tr))
    template <class T, typename = typename std::enable_if<
                           std::is_floating_point<T>::value ||
                           tinysimd::is_vector_floating_point<T>::value>::type>
    inline T Alpha(const T &temp)
    {
        return 1.0 / sqrt(temp / m_Tc);
    }
 
    // Log term term of Peng-Robinson EoS
    template <class T, typename = typename std::enable_if<
                           std::is_floating_point<T>::value ||
                           tinysimd::is_vector_floating_point<T>::value>::type>
    inline T LogTerm(const T &rho)
    {
        return log(1.0 + m_b * rho);
    }
 
    template <class T, typename = typename std::enable_if<
                           std::is_floating_point<T>::value ||
                           tinysimd::is_vector_floating_point<T>::value>::type>
    inline T GetTemperatureKernel(const T &rho, const T &e)
    {
        // First we need to evaluate the log term
        //    ln[1 + b*rho]
        T logTerm = LogTerm(rho);
 
        // The temperature can be expressed as an equation in the form
        //      (T^1/2)^3 + A* T^1/2 + B = 0, which we solve iteratively
        T A = e * (1.0 - m_gamma) / m_gasConstant;
        T B = -3.0 * m_a / (2.0 * m_b * m_gasConstant) * (m_gamma - 1) *
              sqrt(m_Tc) * logTerm;
 
        // Use ideal gas solution as starting guess for iteration
        T sqrtT = sqrt(e * (m_gamma - 1) / m_gasConstant);
        // Newton-Raphson iteration to find T^(1/2)
        T tol                = 1e-6;
        T residual           = 1;
        unsigned int maxIter = 100;
        unsigned int cnt     = 0;
        while (abs(residual) > tol && cnt < maxIter)
        {
            T f      = sqrtT * sqrtT * sqrtT + A * sqrtT + B;
            T df     = 3 * sqrtT * sqrtT + A;
            residual = f / df;
            sqrtT -= residual;
            ++cnt;
        }
        if (cnt == maxIter)
        {
            std::cout << "Newton-Raphson in RedlichKwongEoS::v_GetTemperature "
                         "did not "
                         "converge in "
                      << maxIter << " iterations (residual = " << residual
                      << ")" << std::endl;
        }
 
        // Calculate the temperature
        return sqrtT * sqrtT;
    }
 
    template <class T, typename = typename std::enable_if<
                           std::is_floating_point<T>::value ||
                           tinysimd::is_vector_floating_point<T>::value>::type>
    inline T GetPressureKernel(const T &rho, const T &e)
    {
        T temp    = GetTemperatureKernel(rho, e);
        T oneOrho = 1.0 / rho;
        T p       = m_gasConstant * temp / (oneOrho - m_b) -
              m_a * Alpha(temp) / (oneOrho * (oneOrho + m_b));
        return p;
    }
};
} // namespace Nektar
#endif