xref: /honee/qfunctions/eulervortex.h (revision 704b8bbec5160b50bdbeb899c12e13fec5e0b179)

// Copyright (c) 2017-2022, Lawrence Livermore National Security, LLC and other CEED contributors.
// All Rights Reserved. See the top-level LICENSE and NOTICE files for details.
//
// SPDX-License-Identifier: BSD-2-Clause
//
// This file is part of CEED:  http://github.com/ceed

/// @file
/// Euler traveling vortex initial condition and operator for Navier-Stokes
/// example using PETSc

// Model from:
//   On the Order of Accuracy and Numerical Performance of Two Classes of
//   Finite Volume WENO Schemes, Zhang, Zhang, and Shu (2011).

#ifndef eulervortex_h
#define eulervortex_h

#include <math.h>
#include <ceed.h>
#include "utils.h"

typedef struct EulerContext_ *EulerContext;
struct EulerContext_ {
  CeedScalar center[3];
  CeedScalar curr_time;
  CeedScalar vortex_strength;
  CeedScalar c_tau;
  CeedScalar mean_velocity[3];
  bool implicit;
  int euler_test;
  int stabilization; // See StabilizationType: 0=none, 1=SU, 2=SUPG
};

// *****************************************************************************
// This function sets the initial conditions
//
//   Temperature:
//     T   = 1 - (gamma - 1) vortex_strength**2 exp(1 - r**2) / (8 gamma pi**2)
//   Density:
//     rho = (T/S_vortex)^(1 / (gamma - 1))
//   Pressure:
//     P   = rho * T
//   Velocity:
//     ui  = 1 + vortex_strength exp((1 - r**2)/2.) [yc - y, x - xc] / (2 pi)
//     r   = sqrt( (x - xc)**2 + (y - yc)**2 )
//   Velocity/Momentum Density:
//     Ui  = rho ui
//   Total Energy:
//     E   = P / (gamma - 1) + rho (u u)/2
//
// Constants:
//   cv              ,  Specific heat, constant volume
//   cp              ,  Specific heat, constant pressure
//   vortex_strength ,  Strength of vortex
//   center          ,  Location of bubble center
//   gamma  = cp / cv,  Specific heat ratio
//
// *****************************************************************************

// *****************************************************************************
// This helper function provides support for the exact, time-dependent solution
//   (currently not implemented) and IC formulation for Euler traveling vortex
// *****************************************************************************
CEED_QFUNCTION_HELPER int Exact_Euler(CeedInt dim, CeedScalar time,
                                      const CeedScalar X[], CeedInt Nf, CeedScalar q[],
                                      void *ctx) {
  // Context
  const EulerContext context = (EulerContext)ctx;
  const CeedScalar vortex_strength    = context->vortex_strength;
  const CeedScalar *center            = context->center; // Center of the domain
  const CeedScalar *mean_velocity = context->mean_velocity;

  // Setup
  const CeedScalar gamma = 1.4;
  const CeedScalar cv    = 2.5;
  const CeedScalar R     = 1.;
  const CeedScalar x     = X[0], y = X[1]; // Coordinates
  // Vortex center
  const CeedScalar xc = center[0] + mean_velocity[0] * time;
  const CeedScalar yc = center[1] + mean_velocity[1] * time;

  const CeedScalar x0       = x - xc;
  const CeedScalar y0       = y - yc;
  const CeedScalar r        = sqrt( x0*x0 + y0*y0 );
  const CeedScalar C        = vortex_strength * exp((1. - r*r)/2.) / (2. * M_PI);
  const CeedScalar delta_T  = - (gamma - 1.) * vortex_strength * vortex_strength *
                              exp(1 - r*r) / (8. * gamma * M_PI * M_PI);
  const CeedScalar S_vortex = 1; // no perturbation in the entropy P / rho^gamma
  const CeedScalar S_bubble = (gamma - 1.) * vortex_strength * vortex_strength /
                              (8.*gamma*M_PI*M_PI);
  CeedScalar rho, P, T, E, u[3] = {0.};

  // Initial Conditions
  switch (context->euler_test) {
  case 0: // Traveling vortex
    T = 1 + delta_T;
    // P = rho * T
    // P = S * rho^gamma
    // Solve for rho, then substitute for P
    rho  = pow(T/S_vortex, 1 / (gamma - 1.));
    P    = rho * T;
    u[0] = mean_velocity[0] - C*y0;
    u[1] = mean_velocity[1] + C*x0;

    // Assign exact solution
    q[0] = rho;
    q[1] = rho * u[0];
    q[2] = rho * u[1];
    q[3] = rho * u[2];
    q[4] = P / (gamma - 1.) + rho * (u[0]*u[0] + u[1]*u[1]) / 2.;
    break;
  case 1: // Constant zero velocity, density constant, total energy constant
    rho  = 1.;
    E    = 2.;

    // Assign exact solution
    q[0] = rho;
    q[1] = rho * u[0];
    q[2] = rho * u[1];
    q[3] = rho * u[2];
    q[4] = E;
    break;
  case 2: // Constant nonzero velocity, density constant, total energy constant
    rho  = 1.;
    E    = 2.;
    u[0] = mean_velocity[0];
    u[1] = mean_velocity[1];

    // Assign exact solution
    q[0] = rho;
    q[1] = rho * u[0];
    q[2] = rho * u[1];
    q[3] = rho * u[2];
    q[4] = E;
    break;
  case 3: // Velocity zero, pressure constant
    // (so density and internal energy will be non-constant),
    // but the velocity should stay zero and the bubble won't diffuse
    // (for Euler, where there is no thermal conductivity)
    P    = 1.;
    T    = 1. - S_bubble * exp(1. - r*r);
    rho  = P / (R*T);

    // Assign exact solution
    q[0] = rho;
    q[1] = rho * u[0];
    q[2] = rho * u[1];
    q[3] = rho * u[2];
    q[4] = rho * (cv * T + (u[0]*u[0] + u[1]*u[1])/2.);
    break;
  case 4: // Constant nonzero velocity, pressure constant
    // (so density and internal energy will be non-constant),
    // it should be transported across the domain, but velocity stays constant
    P    = 1.;
    T    = 1. - S_bubble * exp(1. - r*r);
    rho  = P / (R*T);
    u[0] = mean_velocity[0];
    u[1] = mean_velocity[1];

    // Assign exact solution
    q[0] = rho;
    q[1] = rho * u[0];
    q[2] = rho * u[1];
    q[3] = rho * u[2];
    q[4] = rho * (cv * T + (u[0]*u[0] + u[1]*u[1])/2.);
    break;
  case 5: // non-smooth thermal bubble - cylinder
    P    = 1.;
    T = 1. - (r < 1. ? S_bubble : 0.);
    rho  = P / (R*T);
    u[0] = mean_velocity[0];
    u[1] = mean_velocity[1];

    // Assign exact solution
    q[0] = rho;
    q[1] = rho * u[0];
    q[2] = rho * u[1];
    q[3] = rho * u[2];
    q[4] = rho * (cv * T + (u[0]*u[0] + u[1]*u[1])/2.);
    break;
  }
  // Return
  return 0;
}

// *****************************************************************************
// Helper function for computing flux Jacobian
// *****************************************************************************
CEED_QFUNCTION_HELPER void ConvectiveFluxJacobian_Euler(CeedScalar dF[3][5][5],
    const CeedScalar rho, const CeedScalar u[3], const CeedScalar E,
    const CeedScalar gamma) {
  CeedScalar u_sq = u[0]*u[0] + u[1]*u[1] + u[2]*u[2]; // Velocity square
  for (CeedInt i=0; i<3; i++) { // Jacobian matrices for 3 directions
    for (CeedInt j=0; j<3; j++) { // Rows of each Jacobian matrix
      dF[i][j+1][0] = ((i==j) ? ((gamma-1.)*(u_sq/2.)) : 0.) - u[i]*u[j];
      for (CeedInt k=0; k<3; k++) { // Columns of each Jacobian matrix
        dF[i][0][k+1]   = ((i==k) ? 1. : 0.);
        dF[i][j+1][k+1] = ((j==k) ? u[i] : 0.) +
                          ((i==k) ? u[j] : 0.) -
                          ((i==j) ? u[k] : 0.) * (gamma-1.);
        dF[i][4][k+1]   = ((i==k) ? (E*gamma/rho - (gamma-1.)*u_sq/2.) : 0.) -
                          (gamma-1.)*u[i]*u[k];
      }
      dF[i][j+1][4] = ((i==j) ? (gamma-1.) : 0.);
    }
    dF[i][4][0] = u[i] * ((gamma-1.)*u_sq - E*gamma/rho);
    dF[i][4][4] = u[i] * gamma;
  }
}

// *****************************************************************************
// Helper function for computing Tau elements (stabilization constant)
//   Model from:
//     Stabilized Methods for Compressible Flows, Hughes et al 2010
//
//   Spatial criterion #2 - Tau is a 3x3 diagonal matrix
//   Tau[i] = c_tau h[i] Xi(Pe) / rho(A[i]) (no sum)
//
// Where
//   c_tau     = stabilization constant (0.5 is reported as "optimal")
//   h[i]      = 2 length(dxdX[i])
//   Pe        = Peclet number ( Pe = sqrt(u u) / dot(dXdx,u) diffusivity )
//   Xi(Pe)    = coth Pe - 1. / Pe (1. at large local Peclet number )
//   rho(A[i]) = spectral radius of the convective flux Jacobian i,
//               wave speed in direction i
// *****************************************************************************
CEED_QFUNCTION_HELPER void Tau_spatial(CeedScalar Tau_x[3],
                                       const CeedScalar dXdx[3][3], const CeedScalar u[3],
                                       const CeedScalar sound_speed, const CeedScalar c_tau) {
  for (CeedInt i=0; i<3; i++) {
    // length of element in direction i
    CeedScalar h = 2 / sqrt(dXdx[0][i]*dXdx[0][i] + dXdx[1][i]*dXdx[1][i] +
                            dXdx[2][i]*dXdx[2][i]);
    // fastest wave in direction i
    CeedScalar fastest_wave = fabs(u[i]) + sound_speed;
    Tau_x[i] = c_tau * h / fastest_wave;
  }
}

// *****************************************************************************
// This QFunction sets the initial conditions for Euler traveling vortex
// *****************************************************************************
CEED_QFUNCTION(ICsEuler)(void *ctx, CeedInt Q,
                         const CeedScalar *const *in, CeedScalar *const *out) {
  // Inputs
  const CeedScalar (*X)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[0];

  // Outputs
  CeedScalar (*q0)[CEED_Q_VLA] = (CeedScalar(*)[CEED_Q_VLA])out[0];
  const EulerContext context = (EulerContext)ctx;

  CeedPragmaSIMD
  // Quadrature Point Loop
  for (CeedInt i=0; i<Q; i++) {
    const CeedScalar x[] = {X[0][i], X[1][i], X[2][i]};
    CeedScalar q[5] = {0.};

    Exact_Euler(3, context->curr_time, x, 5, q, ctx);

    for (CeedInt j=0; j<5; j++)
      q0[j][i] = q[j];
  } // End of Quadrature Point Loop

  // Return
  return 0;
}

// *****************************************************************************
// This QFunction implements the following formulation of Euler equations
//   with explicit time stepping method
//
// This is 3D Euler for compressible gas dynamics in conservation
//   form with state variables of density, momentum density, and total
//   energy density.
//
// State Variables: q = ( rho, U1, U2, U3, E )
//   rho - Mass Density
//   Ui  - Momentum Density,      Ui = rho ui
//   E   - Total Energy Density,  E  = P / (gamma - 1) + rho (u u)/2
//
// Euler Equations:
//   drho/dt + div( U )                   = 0
//   dU/dt   + div( rho (u x u) + P I3 )  = 0
//   dE/dt   + div( (E + P) u )           = 0
//
// Equation of State:
//   P = (gamma - 1) (E - rho (u u) / 2)
//
// Constants:
//   cv              ,  Specific heat, constant volume
//   cp              ,  Specific heat, constant pressure
//   g               ,  Gravity
//   gamma  = cp / cv,  Specific heat ratio
// *****************************************************************************
CEED_QFUNCTION(Euler)(void *ctx, CeedInt Q,
                      const CeedScalar *const *in, CeedScalar *const *out) {
  // *INDENT-OFF*
  // Inputs
  const CeedScalar (*q)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[0],
                   (*dq)[5][CEED_Q_VLA] = (const CeedScalar(*)[5][CEED_Q_VLA])in[1],
                   (*q_data)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[2];
  // Outputs
  CeedScalar (*v)[CEED_Q_VLA] = (CeedScalar(*)[CEED_Q_VLA])out[0],
             (*dv)[5][CEED_Q_VLA] = (CeedScalar(*)[5][CEED_Q_VLA])out[1];

  EulerContext context = (EulerContext)ctx;
  const CeedScalar c_tau = context->c_tau;
  const CeedScalar gamma = 1.4;

  CeedPragmaSIMD
  // Quadrature Point Loop
  for (CeedInt i=0; i<Q; i++) {
    // *INDENT-OFF*
    // Setup
    // -- Interp in
    const CeedScalar rho        =   q[0][i];
    const CeedScalar u[3]       =  {q[1][i] / rho,
                                    q[2][i] / rho,
                                    q[3][i] / rho
                                   };
    const CeedScalar E          =   q[4][i];
    const CeedScalar drho[3]    =  {dq[0][0][i],
                                    dq[1][0][i],
                                    dq[2][0][i]
                                   };
    const CeedScalar dU[3][3]   = {{dq[0][1][i],
                                    dq[1][1][i],
                                    dq[2][1][i]},
                                   {dq[0][2][i],
                                    dq[1][2][i],
                                    dq[2][2][i]},
                                   {dq[0][3][i],
                                    dq[1][3][i],
                                    dq[2][3][i]}
                                  };
    const CeedScalar dE[3]      =  {dq[0][4][i],
                                    dq[1][4][i],
                                    dq[2][4][i]
                                   };
    // -- Interp-to-Interp q_data
    const CeedScalar wdetJ      =   q_data[0][i];
    // -- Interp-to-Grad q_data
    // ---- Inverse of change of coordinate matrix: X_i,j
    // *INDENT-OFF*
    const CeedScalar dXdx[3][3] = {{q_data[1][i],
                                    q_data[2][i],
                                    q_data[3][i]},
                                   {q_data[4][i],
                                    q_data[5][i],
                                    q_data[6][i]},
                                   {q_data[7][i],
                                    q_data[8][i],
                                    q_data[9][i]}
                                  };
    // *INDENT-ON*
    // dU/dx
    CeedScalar drhodx[3] = {0.};
    CeedScalar dEdx[3] = {0.};
    CeedScalar dUdx[3][3] = {{0.}};
    CeedScalar dXdxdXdxT[3][3] = {{0.}};
    for (CeedInt j=0; j<3; j++) {
      for (CeedInt k=0; k<3; k++) {
        drhodx[j] += drho[k] * dXdx[k][j];
        dEdx[j] += dE[k] * dXdx[k][j];
        for (CeedInt l=0; l<3; l++) {
          dUdx[j][k] += dU[j][l] * dXdx[l][k];
          dXdxdXdxT[j][k] += dXdx[j][l]*dXdx[k][l];  //dXdx_j,k * dXdx_k,j
        }
      }
    }
    // Pressure
    const CeedScalar
    E_kinetic  = 0.5 * rho * (u[0]*u[0] + u[1]*u[1] + u[2]*u[2]),
    E_internal = E - E_kinetic,
    P          = E_internal * (gamma - 1.); // P = pressure

    // The Physics
    // Zero v and dv so all future terms can safely sum into it
    for (CeedInt j=0; j<5; j++) {
      v[j][i] = 0.;
      for (CeedInt k=0; k<3; k++)
        dv[k][j][i] = 0.;
    }

    // -- Density
    // ---- u rho
    for (CeedInt j=0; j<3; j++)
      dv[j][0][i]  += wdetJ*(rho*u[0]*dXdx[j][0] + rho*u[1]*dXdx[j][1] +
                             rho*u[2]*dXdx[j][2]);
    // -- Momentum
    // ---- rho (u x u) + P I3
    for (CeedInt j=0; j<3; j++)
      for (CeedInt k=0; k<3; k++)
        dv[k][j+1][i]  += wdetJ*((rho*u[j]*u[0] + (j==0?P:0.))*dXdx[k][0] +
                                 (rho*u[j]*u[1] + (j==1?P:0.))*dXdx[k][1] +
                                 (rho*u[j]*u[2] + (j==2?P:0.))*dXdx[k][2]);
    // -- Total Energy Density
    // ---- (E + P) u
    for (CeedInt j=0; j<3; j++)
      dv[j][4][i]  += wdetJ * (E + P) * (u[0]*dXdx[j][0] + u[1]*dXdx[j][1] +
                                         u[2]*dXdx[j][2]);

    // --Stabilization terms
    // ---- jacob_F_conv[3][5][5] = dF(convective)/dq at each direction
    CeedScalar jacob_F_conv[3][5][5] = {{{0.}}};
    ConvectiveFluxJacobian_Euler(jacob_F_conv, rho, u, E, gamma);

    // ---- dqdx collects drhodx, dUdx and dEdx in one vector
    CeedScalar dqdx[5][3];
    for (CeedInt j=0; j<3; j++) {
      dqdx[0][j] = drhodx[j];
      dqdx[4][j] = dEdx[j];
      for (CeedInt k=0; k<3; k++)
        dqdx[k+1][j] = dUdx[k][j];
    }

    // ---- strong_conv = dF/dq * dq/dx    (Strong convection)
    CeedScalar strong_conv[5] = {0.};
    for (CeedInt j=0; j<3; j++)
      for (CeedInt k=0; k<5; k++)
        for (CeedInt l=0; l<5; l++)
          strong_conv[k] += jacob_F_conv[j][k][l] * dqdx[l][j];

    // Stabilization
    // -- Tau elements
    const CeedScalar sound_speed = sqrt(gamma * P / rho);
    CeedScalar Tau_x[3] = {0.};
    Tau_spatial(Tau_x, dXdx, u, sound_speed, c_tau);

    // -- Stabilization method: none or SU
    CeedScalar stab[5][3] = {{0.}};
    switch (context->stabilization) {
    case 0:        // Galerkin
      break;
    case 1:        // SU
      for (CeedInt j=0; j<3; j++)
        for (CeedInt k=0; k<5; k++)
          for (CeedInt l=0; l<5; l++)
            stab[k][j] += jacob_F_conv[j][k][l] * Tau_x[j] * strong_conv[l];

      for (CeedInt j=0; j<5; j++)
        for (CeedInt k=0; k<3; k++)
          dv[k][j][i] -= wdetJ*(stab[j][0] * dXdx[k][0] +
                                stab[j][1] * dXdx[k][1] +
                                stab[j][2] * dXdx[k][2]);
      break;
    case 2:        // SUPG is not implemented for explicit scheme
      break;
    }

  } // End Quadrature Point Loop

  // Return
  return 0;
}

// *****************************************************************************
// This QFunction implements the Euler equations with (mentioned above)
//   with implicit time stepping method
//
// *****************************************************************************
CEED_QFUNCTION(IFunction_Euler)(void *ctx, CeedInt Q,
                                const CeedScalar *const *in, CeedScalar *const *out) {
  // *INDENT-OFF*
  // Inputs
  const CeedScalar (*q)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[0],
                   (*dq)[5][CEED_Q_VLA] = (const CeedScalar(*)[5][CEED_Q_VLA])in[1],
                   (*q_dot)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[2],
                   (*q_data)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[3];
  // Outputs
  CeedScalar (*v)[CEED_Q_VLA] = (CeedScalar(*)[CEED_Q_VLA])out[0],
             (*dv)[5][CEED_Q_VLA] = (CeedScalar(*)[5][CEED_Q_VLA])out[1];

  EulerContext context = (EulerContext)ctx;
  const CeedScalar c_tau = context->c_tau;
  const CeedScalar gamma = 1.4;

  CeedPragmaSIMD
  // Quadrature Point Loop
  for (CeedInt i=0; i<Q; i++) {
    // *INDENT-OFF*
    // Setup
    // -- Interp in
    const CeedScalar rho        =   q[0][i];
    const CeedScalar u[3]       =  {q[1][i] / rho,
                                    q[2][i] / rho,
                                    q[3][i] / rho
                                   };
    const CeedScalar E          =   q[4][i];
    const CeedScalar drho[3]    =  {dq[0][0][i],
                                    dq[1][0][i],
                                    dq[2][0][i]
                                   };
    const CeedScalar dU[3][3]   = {{dq[0][1][i],
                                    dq[1][1][i],
                                    dq[2][1][i]},
                                   {dq[0][2][i],
                                    dq[1][2][i],
                                    dq[2][2][i]},
                                   {dq[0][3][i],
                                    dq[1][3][i],
                                    dq[2][3][i]}
                                  };
    const CeedScalar dE[3]      =  {dq[0][4][i],
                                    dq[1][4][i],
                                    dq[2][4][i]
                                   };
    // -- Interp-to-Interp q_data
    const CeedScalar wdetJ      =   q_data[0][i];
    // -- Interp-to-Grad q_data
    // ---- Inverse of change of coordinate matrix: X_i,j
    // *INDENT-OFF*
    const CeedScalar dXdx[3][3] = {{q_data[1][i],
                                    q_data[2][i],
                                    q_data[3][i]},
                                   {q_data[4][i],
                                    q_data[5][i],
                                    q_data[6][i]},
                                   {q_data[7][i],
                                    q_data[8][i],
                                    q_data[9][i]}
                                  };
    // *INDENT-ON*
    // dU/dx
    CeedScalar drhodx[3] = {0.};
    CeedScalar dEdx[3] = {0.};
    CeedScalar dUdx[3][3] = {{0.}};
    CeedScalar dXdxdXdxT[3][3] = {{0.}};
    for (CeedInt j=0; j<3; j++) {
      for (CeedInt k=0; k<3; k++) {
        drhodx[j] += drho[k] * dXdx[k][j];
        dEdx[j] += dE[k] * dXdx[k][j];
        for (CeedInt l=0; l<3; l++) {
          dUdx[j][k] += dU[j][l] * dXdx[l][k];
          dXdxdXdxT[j][k] += dXdx[j][l]*dXdx[k][l];  //dXdx_j,k * dXdx_k,j
        }
      }
    }
    const CeedScalar
    E_kinetic  = 0.5 * rho * (u[0]*u[0] + u[1]*u[1] + u[2]*u[2]),
    E_internal = E - E_kinetic,
    P          = E_internal * (gamma - 1.); // P = pressure

    // The Physics
    // Zero v and dv so all future terms can safely sum into it
    for (CeedInt j=0; j<5; j++) {
      v[j][i] = 0.;
      for (CeedInt k=0; k<3; k++)
        dv[k][j][i] = 0.;
    }
    //-----mass matrix
    for (CeedInt j=0; j<5; j++)
      v[j][i] += wdetJ*q_dot[j][i];

    // -- Density
    // ---- u rho
    for (CeedInt j=0; j<3; j++)
      dv[j][0][i]  -= wdetJ*(rho*u[0]*dXdx[j][0] + rho*u[1]*dXdx[j][1] +
                             rho*u[2]*dXdx[j][2]);
    // -- Momentum
    // ---- rho (u x u) + P I3
    for (CeedInt j=0; j<3; j++)
      for (CeedInt k=0; k<3; k++)
        dv[k][j+1][i]  -= wdetJ*((rho*u[j]*u[0] + (j==0?P:0.))*dXdx[k][0] +
                                 (rho*u[j]*u[1] + (j==1?P:0.))*dXdx[k][1] +
                                 (rho*u[j]*u[2] + (j==2?P:0.))*dXdx[k][2]);
    // -- Total Energy Density
    // ---- (E + P) u
    for (CeedInt j=0; j<3; j++)
      dv[j][4][i]  -= wdetJ * (E + P) * (u[0]*dXdx[j][0] + u[1]*dXdx[j][1] +
                                         u[2]*dXdx[j][2]);

    // -- Stabilization terms
    // ---- jacob_F_conv[3][5][5] = dF(convective)/dq at each direction
    CeedScalar jacob_F_conv[3][5][5] = {{{0.}}};
    ConvectiveFluxJacobian_Euler(jacob_F_conv, rho, u, E, gamma);

    // ---- dqdx collects drhodx, dUdx and dEdx in one vector
    CeedScalar dqdx[5][3];
    for (CeedInt j=0; j<3; j++) {
      dqdx[0][j] = drhodx[j];
      dqdx[4][j] = dEdx[j];
      for (CeedInt k=0; k<3; k++)
        dqdx[k+1][j] = dUdx[k][j];
    }

    // ---- strong_conv = dF/dq * dq/dx    (Strong convection)
    CeedScalar strong_conv[5] = {0.};
    for (CeedInt j=0; j<3; j++)
      for (CeedInt k=0; k<5; k++)
        for (CeedInt l=0; l<5; l++)
          strong_conv[k] += jacob_F_conv[j][k][l] * dqdx[l][j];

    // ---- Strong residual
    CeedScalar strong_res[5];
    for (CeedInt j=0; j<5; j++)
      strong_res[j] = q_dot[j][i] + strong_conv[j];

    // Stabilization
    // -- Tau elements
    const CeedScalar sound_speed = sqrt(gamma * P / rho);
    CeedScalar Tau_x[3] = {0.};
    Tau_spatial(Tau_x, dXdx, u, sound_speed, c_tau);

    // -- Stabilization method: none, SU, or SUPG
    CeedScalar stab[5][3] = {{0.}};
    switch (context->stabilization) {
    case 0:        // Galerkin
      break;
    case 1:        // SU
      for (CeedInt j=0; j<3; j++)
        for (CeedInt k=0; k<5; k++)
          for (CeedInt l=0; l<5; l++)
            stab[k][j] += jacob_F_conv[j][k][l] * Tau_x[j] * strong_conv[l];

      for (CeedInt j=0; j<5; j++)
        for (CeedInt k=0; k<3; k++)
          dv[k][j][i] += wdetJ*(stab[j][0] * dXdx[k][0] +
                                stab[j][1] * dXdx[k][1] +
                                stab[j][2] * dXdx[k][2]);
      break;
    case 2:        // SUPG
      for (CeedInt j=0; j<3; j++)
        for (CeedInt k=0; k<5; k++)
          for (CeedInt l=0; l<5; l++)
            stab[k][j] = jacob_F_conv[j][k][l] * Tau_x[j] * strong_res[l];

      for (CeedInt j=0; j<5; j++)
        for (CeedInt k=0; k<3; k++)
          dv[k][j][i] += wdetJ*(stab[j][0] * dXdx[k][0] +
                                stab[j][1] * dXdx[k][1] +
                                stab[j][2] * dXdx[k][2]);
      break;
    }
  } // End Quadrature Point Loop

  // Return
  return 0;
}
// *****************************************************************************
// This QFunction sets the inflow boundary conditions for
//   the traveling vortex problem.
//
//  Prescribed T_inlet and P_inlet are converted to conservative variables
//      and applied weakly.
//
// *****************************************************************************
CEED_QFUNCTION(TravelingVortex_Inflow)(void *ctx, CeedInt Q,
                                       const CeedScalar *const *in,
                                       CeedScalar *const *out) {
  // *INDENT-OFF*
  // Inputs
  const CeedScalar (*q_data_sur)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[2];
  // Outputs
  CeedScalar (*v)[CEED_Q_VLA] = (CeedScalar(*)[CEED_Q_VLA])out[0];
  // *INDENT-ON*
  EulerContext context = (EulerContext)ctx;
  const int euler_test      = context->euler_test;
  const bool implicit       = context->implicit;
  CeedScalar *mean_velocity = context->mean_velocity;
  const CeedScalar cv    = 2.5;
  const CeedScalar R     = 1.;
  CeedScalar T_inlet;
  CeedScalar P_inlet;

  // For test cases 1 and 3 the background velocity is zero
  if (euler_test == 1 || euler_test == 3)
    for (CeedInt i=0; i<3; i++) mean_velocity[i] = 0.;

  // For test cases 1 and 2, T_inlet = T_inlet = 0.4
  if (euler_test == 1 || euler_test == 2) T_inlet = P_inlet = .4;
  else T_inlet = P_inlet = 1.;

  CeedPragmaSIMD
  // Quadrature Point Loop
  for (CeedInt i=0; i<Q; i++) {
    // Setup
    // -- Interp-to-Interp q_data
    // For explicit mode, the surface integral is on the RHS of ODE q_dot = f(q).
    // For implicit mode, it gets pulled to the LHS of implicit ODE/DAE g(q_dot, q).
    // We can effect this by swapping the sign on this weight
    const CeedScalar wdetJb  = (implicit ? -1. : 1.) * q_data_sur[0][i];
    // ---- Normal vect
    const CeedScalar norm[3] = {q_data_sur[1][i],
                                q_data_sur[2][i],
                                q_data_sur[3][i]
                               };

    // face_normal = Normal vector of the face
    const CeedScalar face_normal = norm[0]*mean_velocity[0] +
                                   norm[1]*mean_velocity[1] +
                                   norm[2]*mean_velocity[2];
    // The Physics
    // Zero v so all future terms can safely sum into it
    for (CeedInt j=0; j<5; j++) v[j][i] = 0.;

    // Implementing in/outflow BCs
    if (face_normal > 0) {
    } else { // inflow
      const CeedScalar rho_inlet = P_inlet/(R*T_inlet);
      const CeedScalar E_kinetic_inlet = (mean_velocity[0]*mean_velocity[0] +
                                          mean_velocity[1]*mean_velocity[1]) / 2.;
      // incoming total energy
      const CeedScalar E_inlet = rho_inlet * (cv * T_inlet + E_kinetic_inlet);

      // The Physics
      // -- Density
      v[0][i] -= wdetJb * rho_inlet * face_normal;

      // -- Momentum
      for (CeedInt j=0; j<3; j++)
        v[j+1][i] -= wdetJb *(rho_inlet * face_normal * mean_velocity[j] +
                              norm[j] * P_inlet);

      // -- Total Energy Density
      v[4][i] -= wdetJb * face_normal * (E_inlet + P_inlet);
    }

  } // End Quadrature Point Loop
  return 0;
}

// *****************************************************************************
// This QFunction sets the outflow boundary conditions for
//   the Euler solver.
//
//  Outflow BCs:
//    The validity of the weak form of the governing equations is
//      extended to the outflow.
//
// *****************************************************************************
CEED_QFUNCTION(Euler_Outflow)(void *ctx, CeedInt Q,
                              const CeedScalar *const *in,
                              CeedScalar *const *out) {
  // *INDENT-OFF*
  // Inputs
  const CeedScalar (*q)[CEED_Q_VLA]          = (const CeedScalar(*)[CEED_Q_VLA])in[0],
                   (*q_data_sur)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[2];
  // Outputs
  CeedScalar (*v)[CEED_Q_VLA] = (CeedScalar(*)[CEED_Q_VLA])out[0];
  // *INDENT-ON*
  EulerContext context = (EulerContext)ctx;
  const bool implicit       = context->implicit;
  CeedScalar *mean_velocity = context->mean_velocity;

  const CeedScalar gamma = 1.4;

  CeedPragmaSIMD
  // Quadrature Point Loop
  for (CeedInt i=0; i<Q; i++) {
    // Setup
    // -- Interp in
    const CeedScalar rho      =  q[0][i];
    const CeedScalar u[3]     = {q[1][i] / rho,
                                 q[2][i] / rho,
                                 q[3][i] / rho
                                };
    const CeedScalar E        =  q[4][i];

    // -- Interp-to-Interp q_data
    // For explicit mode, the surface integral is on the RHS of ODE q_dot = f(q).
    // For implicit mode, it gets pulled to the LHS of implicit ODE/DAE g(q_dot, q).
    // We can effect this by swapping the sign on this weight
    const CeedScalar wdetJb     =   (implicit ? -1. : 1.) * q_data_sur[0][i];
    // ---- Normal vectors
    const CeedScalar norm[3]    =   {q_data_sur[1][i],
                                     q_data_sur[2][i],
                                     q_data_sur[3][i]
                                    };

    // face_normal = Normal vector of the face
    const CeedScalar face_normal = norm[0]*mean_velocity[0] +
                                   norm[1]*mean_velocity[1] +
                                   norm[2]*mean_velocity[2];
    // The Physics
    // Zero v so all future terms can safely sum into it
    for (CeedInt j=0; j<5; j++) v[j][i] = 0;

    // Implementing in/outflow BCs
    if (face_normal > 0) { // outflow
      const CeedScalar E_kinetic = (u[0]*u[0] + u[1]*u[1]) / 2.;
      const CeedScalar P         = (E - E_kinetic * rho) * (gamma - 1.); // pressure
      const CeedScalar u_normal  = norm[0]*u[0] + norm[1]*u[1] +
                                   norm[2]*u[2]; // Normal velocity
      // The Physics
      // -- Density
      v[0][i] -= wdetJb * rho * u_normal;

      // -- Momentum
      for (CeedInt j=0; j<3; j++)
        v[j+1][i] -= wdetJb *(rho * u_normal * u[j] + norm[j] * P);

      // -- Total Energy Density
      v[4][i] -= wdetJb * u_normal * (E + P);
    }
  } // End Quadrature Point Loop
  return 0;
}

// *****************************************************************************

#endif // eulervortex_h