GlobalPhysicalVariables Namespace Reference

Namespace for physical parameters. More...

Variables

double Re = 301.0
 Reynolds number. More...
 
double ReSt = 301.0
 Product of Reynolds and Strouhal numbers. More...
 
double ReInvFr = 0.0
 Product of Rynolds number and inverse of Froude number. More...
 
double Gamma = 1.0
 Aspect ratio (cylinder height / cylinder radius) More...
 
int k = 2
 Azimuthal mode number k in e^ik(theta) decomposition. More...
 
Vector< doubleG (3)
 Direction of gravity. More...
 
double St = 1.0
 Strouhal number. More...
 
double InvFr = 0.0
 Inverse of Froude number. More...
 
double Re_current
 
double ReSt_current
 
double ReInvFr_current
 
double Re_lower_limit = 300
 Loop information. More...
 
double Re_upper_limit = 302
 
unsigned Nparam_steps = 5
 
double MMC_Re_current
 
double MMC_Re_lower_limit = 20.93
 Loop information. More...
 
double MMC_Re_upper_limit = 20.94
 
double AngularFrequency = 10.58
 Angular frequency of outer cylinder rotation (omega = 2*gamma^2) More...
 
double Epsilon = 0.9
 Dimensionless modulation amplitude (epsilon) More...
 
double Eta = 0.88
 Radius ratio (radius of inner cylinder / radius of outer cylinder) More...
 
double a = 3.2
 Wavenumber of azimuthal waves e^iaz. More...
 
double Viscosity_Ratio = 0.1
 
double Density_Ratio = 1.0
 
double Ca = 1.0
 Capillary number. More...
 
Vector< intVector_of_azimuthal_mode_numbers
 Vector of azimuthal mode numbers to investigate. More...
 

Detailed Description

Namespace for physical parameters.

Variable Documentation

◆ a

double GlobalPhysicalVariables::a = 3.2

Wavenumber of azimuthal waves e^iaz.

Referenced by main().

◆ AngularFrequency

double GlobalPhysicalVariables::AngularFrequency = 10.58

Angular frequency of outer cylinder rotation (omega = 2*gamma^2)

Referenced by main(), and BaseStateProblem< BASE_ELEMENT >::set_boundary_conditions().

◆ Ca

double GlobalPhysicalVariables::Ca = 1.0

◆ Density_Ratio

double GlobalPhysicalVariables::Density_Ratio = 1.0

Ratio of density in upper fluid to density in lower fluid. Reynolds number etc. is based on density in lower fluid.

Referenced by BaseStateProblem< BASE_ELEMENT >::BaseStateProblem(), and PerturbedStateProblem< BASE_ELEMENT, PERTURBED_ELEMENT >::PerturbedStateProblem().

◆ Epsilon

◆ Eta

double GlobalPhysicalVariables::Eta = 0.88

Radius ratio (radius of inner cylinder / radius of outer cylinder)

Referenced by main(), and BaseStateProblem< BASE_ELEMENT >::set_boundary_conditions().

◆ G

◆ Gamma

double GlobalPhysicalVariables::Gamma = 1.0

Aspect ratio (cylinder height / cylinder radius)

Referenced by oomph::RefineableSpaceTimeNavierStokesEquations< DIM >::fill_in_generic_residual_contribution_nst(), oomph::RefineableSpaceTimeNavierStokesMixedOrderEquations< DIM >::fill_in_generic_residual_contribution_nst(), oomph::SpaceTimeNavierStokesEquations< DIM >::fill_in_generic_residual_contribution_nst(), oomph::SpaceTimeNavierStokesMixedOrderEquations< DIM >::fill_in_generic_residual_contribution_nst(), oomph::GeneralisedNewtonianNavierStokesEquations< DIM >::fill_in_generic_residual_contribution_nst(), oomph::RefineableGeneralisedNewtonianNavierStokesEquations< DIM >::fill_in_generic_residual_contribution_nst(), oomph::NavierStokesEquations< DIM >::fill_in_generic_residual_contribution_nst(), oomph::RefineableNavierStokesEquations< DIM >::fill_in_generic_residual_contribution_nst(), oomph::NavierStokesElementWithSingularity< BASIC_NAVIER_STOKES_ELEMENT >::fill_in_generic_residual_contribution_wrapped_nst(), oomph::GeneralisedNewtonianNavierStokesEquations< DIM >::get_dresidual_dnodal_coordinates(), oomph::RefineableGeneralisedNewtonianNavierStokesEquations< DIM >::get_dresidual_dnodal_coordinates(), oomph::NavierStokesEquations< DIM >::get_dresidual_dnodal_coordinates(), oomph::RefineableNavierStokesEquations< DIM >::get_dresidual_dnodal_coordinates(), oomph::SpaceTimeNavierStokesEquations< DIM >::get_dresidual_dnodal_coordinates(), oomph::RefineableSpaceTimeNavierStokesEquations< DIM >::get_dresidual_dnodal_coordinates(), RachelsAdvectionDiffusion::get_exact_u(), Global::initial_left(), Global::initial_right(), main(), RefineablePorousChannelProblem< ELEMENT >::RefineablePorousChannelProblem(), RotatingProblem< ELEMENT >::RotatingProblem(), SteadyCurvedTubeProblem< ELEMENT >::SteadyCurvedTubeProblem(), SteadyHelicalProblem< ELEMENT >::SteadyHelicalProblem(), SteadyTubeProblem< ELEMENT >::SteadyTubeProblem(), TorusProblem< ELEMENT >::TorusProblem(), and UnstructuredTorusProblem< ELEMENT >::UnstructuredTorusProblem().

◆ InvFr

double GlobalPhysicalVariables::InvFr = 0.0

Inverse of Froude number.

Referenced by main().

◆ k

◆ MMC_Re_current

double GlobalPhysicalVariables::MMC_Re_current

◆ MMC_Re_lower_limit

double GlobalPhysicalVariables::MMC_Re_lower_limit = 20.93

Loop information.

Referenced by main().

◆ MMC_Re_upper_limit

double GlobalPhysicalVariables::MMC_Re_upper_limit = 20.94

Referenced by main().

◆ Nparam_steps

unsigned GlobalPhysicalVariables::Nparam_steps = 5

Referenced by main().

◆ Re

double GlobalPhysicalVariables::Re = 301.0

Reynolds number.

Referenced by AirwayReopeningProblem< ELEMENT >::actions_after_change_in_global_parameter(), oomph::SphericalNavierStokesEquations::actual(), oomph::SphericalNavierStokesEquations::actual_dr(), oomph::SphericalNavierStokesEquations::actual_dth(), FlowAroundCylinderProblem< ELEMENT >::add_eigenproblem(), SSPorousChannelEquations::add_generic_residual_contribution(), BaseStateProblem< BASE_ELEMENT >::BaseStateProblem(), InclinedPlaneProblem< ELEMENT, INTERFACE_ELEMENT >::complete_build(), AirwayReopeningProblem< ELEMENT >::dump(), oomph::PolarNavierStokesEquations::fill_in_generic_residual_contribution(), oomph::RefineablePolarNavierStokesEquations::fill_in_generic_residual_contribution(), RotatingProblem< ELEMENT >::finish_problem_setup(), RefineableRotatingCylinderProblem< ELEMENT >::finish_problem_setup(), PerturbationSolution::full_soln(), Global_Physical_Variables::get_exact_u(), PolarNSProblem< ELEMENT >::header(), main(), AirwayReopeningProblem< ELEMENT >::parameter_study(), GlobalParameters::parameter_to_string(), PerturbedStateProblem< BASE_ELEMENT, PERTURBED_ELEMENT >::PerturbedStateProblem(), AirwayReopeningProblem< ELEMENT >::read(), Global_Parameters::set_parameters(), Global_Physical_Variables::set_params(), RotatingProblem< ELEMENT >::solve_system(), TorusProblem< ELEMENT >::solve_system(), InclinedPlaneProblem< ELEMENT, INTERFACE_ELEMENT >::timestep(), TorusProblem< ELEMENT >::TorusProblem(), UniformTranspiration< ELEMENT >::UniformTranspiration(), UnstructuredTorusProblem< ELEMENT >::UnstructuredTorusProblem(), Global_Physical_Variables::update_dependent_parameters(), GlobalParameters::update_physical_parameters(), and GlobalParameters::update_simulation_parameters().

◆ Re_current

◆ Re_lower_limit

double GlobalPhysicalVariables::Re_lower_limit = 300

Loop information.

Referenced by main().

◆ Re_upper_limit

double GlobalPhysicalVariables::Re_upper_limit = 302

Referenced by main().

◆ ReInvFr

◆ ReInvFr_current

double GlobalPhysicalVariables::ReInvFr_current

◆ ReSt

◆ ReSt_current

◆ St

double GlobalPhysicalVariables::St = 1.0

◆ Vector_of_azimuthal_mode_numbers

Vector<int> GlobalPhysicalVariables::Vector_of_azimuthal_mode_numbers

Vector of azimuthal mode numbers to investigate.

Referenced by main().

◆ Viscosity_Ratio

double GlobalPhysicalVariables::Viscosity_Ratio = 0.1

Ratio of viscosity in upper fluid to viscosity in lower fluid. Reynolds number etc. is based on viscosity in lower fluid.

Referenced by BaseStateProblem< BASE_ELEMENT >::BaseStateProblem(), and PerturbedStateProblem< BASE_ELEMENT, PERTURBED_ELEMENT >::PerturbedStateProblem().