ASSERTION in Function

Altair Forum User
Altair Forum User
Altair Employee
edited October 2020 in Community Q&A

when i change the turbulence model from Spllart almarras to K omega i am getting the below mentioned error.Anyone Can u please let me know what i should do to eliminate this error

 

acuSolve: ---------------------- Input Phase --------------------------
acuSolve: Input CPU/Elapse time      = 4.749000e+000 5.984000e+000 Sec
acuSolve: Input Memory Usage         = 1.075133e+003 Mbytes
acuSolve: ---------------------- Begin Time Step ----------------------
acuSolve: *** ASSERTION in Function <nbcSetTwf> File <nbc.c> Line <1275>
acuSolve: *** Internal error
acuRun: *** ERROR: error occurred executing acuSolve
acuRun: Mon Mar 24 16:35:28 2014
 

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Answers

  • cfdguru
    cfdguru New Altair Community Member
    edited March 2014

    What version of AcuSolve are you using?  Also, is it possible to upload your input file?  This error typically means there is something drastically wrong with the model set up somewhere.

  • Altair Forum User
    Altair Forum User
    Altair Employee
    edited March 2014

    acuRun: Mon Mar 24 16:44:32 2014
    acuRun: acuRun
    acuRun: Processing run 9 ...
    acuRun: Hostname = B2WS0468
    acuRun: Release  = 12.0.310
    acuRun: Reseting message_passing_type to none
    acuRun: Add D:/Tools/Altair/12.0/acusolve/win64/bin to PATH
    acuRun: set PATH=D:/Tools/Altair/12.0/acusolve/win64/bin;D:\Tools\Altair\12.0\acusolve\win64\bin;D:\Tools\Altair\12.0\acusolve\win64\base\bin;D:\Tools\Altair\12.0\acusolve\win64\base\DLLs;D:\Tools\Altair\12.0\acusolve\win64\base\Lib\site-packages;D:\Tools\Altair\12.0\acusolve\win64\JMAG;D:\Tools\Altair\12.0\acusolve\win64\abaqus-odb\lib;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\Program Files\Intel\DMIX;C:\IFOR\WIN\BIN;C:\IFOR\WIN\BIN\EN_US;D:\Tools\Perl\bin;D:\Tools\Altair\12.0\acusolve\win64\perl\bin;D:\Tools\Altair\12.0\acusolve\win64\perl\bin
    acuRun: Run acuPrep ...
    acuRun: D:/Tools/Altair/12.0/acusolve/win64/bin/acuPrep.exe -nst 1
    acuPrep:                         Date = Mon Mar 24 16:44:32 2014
    acuPrep:                      Problem = CFD-sat
    acuPrep:                          Run = 9
    acuPrep:                     Hostname = B2WS0468
    acuPrep:                     Platform = Whistler 5.2 unknown
    acuPrep:                      Machine = win64
    acuPrep:                      Release = 12.0.310
    acuPrep:                 Release date = Aug 14 2013
    acuPrep:         Number of subdomains = 1
    acuPrep:            Number of threads = 1
    acuPrep:            Working directory = ACUSIM.DIR
    acuPrep: ------------------------------------------------------------------
    acuPrep: Reading ANALYSIS
    acuPrep: Reading EQUATION
    acuPrep: Reading AUTO_SOLUTION_STRATEGY
    acuPrep: Processing AUTO_SOLUTION_STRATEGY
    acuPrep: AUTO_SOLUTION_STRATEGY: creating and including 'CFD-sat.ss.inc' ...
    acuPrep: Reading TIME_SEQUENCE
    acuPrep: Reading STAGGER( 'temperature_flow' )
    acuPrep: Reading STAGGER( 'eddy_frequency' )
    acuPrep: Reading STAGGER( 'kinetic_energy' )
    acuPrep: Reading TIME_INCREMENT
    acuPrep: Reading TIME_INTEGRATION
    acuPrep: Reading LINEAR_SOLVER_PARAMETERS
    acuPrep: Reading CONVERGENCE_CHECK_PARAMETERS
    acuPrep: Reading ALGEBRAIC_MULTIGRID_PARAMETERS
    acuPrep: Reading MATERIAL_MODEL( 'Air' )
    acuPrep: Reading DENSITY_MODEL( 'Air' )
    acuPrep: Reading VISCOSITY_MODEL( 'Air' )
    acuPrep: Reading SPECIFIC_HEAT_MODEL( 'Air' )
    acuPrep: Reading CONDUCTIVITY_MODEL( 'Air' )
    acuPrep: Reading POROSITY_MODEL( 'Air' )
    acuPrep: Reading MATERIAL_MODEL( 'Aluminum' )
    acuPrep: Reading DENSITY_MODEL( 'Aluminum' )
    acuPrep: Reading SPECIFIC_HEAT_MODEL( 'Aluminum' )
    acuPrep: Reading CONDUCTIVITY_MODEL( 'Aluminum' )
    acuPrep: Reading BODY_FORCE( 'Gravity' )
    acuPrep: Reading GRAVITY( 'Gravity' )
    acuPrep: Reading MASS_HEAT_SOURCE( 'Gravity' )
    acuPrep: Reading BODY_FORCE( 'Heatsource' )
    acuPrep: Reading VOLUME_HEAT_SOURCE( 'Heatsource' )
    acuPrep: Reading FWH_OUTPUT
    acuPrep: Reading NODAL_OUTPUT
    acuPrep: Reading DERIVED_QUANTITY_OUTPUT
    acuPrep: Reading RUNNING_AVERAGE_OUTPUT
    acuPrep: Reading TIME_AVERAGE_OUTPUT
    acuPrep: Reading ERROR_ESTIMATOR_OUTPUT
    acuPrep: Reading RESTART_OUTPUT
    acuPrep: Reading NODAL_RESIDUAL_OUTPUT
    acuPrep: Reading NODAL_INITIAL_CONDITION( pressure )
    acuPrep: Reading NODAL_INITIAL_CONDITION( velocity )
    acuPrep: Reading NODAL_INITIAL_CONDITION( temperature )
    acuPrep: Reading NODAL_INITIAL_CONDITION( eddy_frequency )
    acuPrep: Reading NODAL_INITIAL_CONDITION( kinetic_energy )
    acuPrep: Reading COORDINATE
    acuPrep: Reading ELEMENT_SET( 'Fluid' )
    acuPrep: Reading ELEMENT_SET( 'solid' )
    acuPrep: Reading SIMPLE_BOUNDARY_CONDITION( 'Heatsource' )
    acuPrep: Reading SURFACE_OUTPUT( 'Heatsource' )
    acuPrep: Reading SIMPLE_BOUNDARY_CONDITION( 'Outlet' )
    acuPrep: Reading SURFACE_OUTPUT( 'Outlet' )
    acuPrep: Reading SIMPLE_BOUNDARY_CONDITION( 'inlet' )
    acuPrep: Reading SURFACE_OUTPUT( 'inlet' )
    acuPrep: Reading SIMPLE_BOUNDARY_CONDITION( 'wall' )
    acuPrep: Reading SURFACE_OUTPUT( 'wall' )
    acuPrep: Reading RUN
    acuPrep: Processing RUN
    acuPrep: Processing ANALYSIS
    acuPrep: Processing EQUATION
    acuPrep: Processing USER_GLOBAL_DATA( 'none' )
    acuPrep: Processing MULTIPLIER_FUNCTION( 'none' )
    acuPrep: Processing RADIATION
    acuPrep: Processing SOLAR_RADIATION
    acuPrep: Processing PARTICLE_TRACE
    acuPrep: Processing EXTERNAL_CODE
    acuPrep: Processing REFERENCE_FRAME( 'none' )
    acuPrep: Processing MESH_MOTION( 'none' )
    acuPrep: Processing TIME_SEQUENCE
    acuPrep: Processing STAGGER( 'temperature_flow' )
    acuPrep: Processing STAGGER( 'eddy_frequency' )
    acuPrep: Processing STAGGER( 'kinetic_energy' )
    acuPrep: Processing TIME_INCREMENT
    acuPrep: Processing CONVERGENCE_CHECK_PARAMETERS
    acuPrep: Processing ALGEBRAIC_MULTIGRID_PARAMETERS
    acuPrep: Processing TIME_INTEGRATION
    acuPrep: Processing LINEAR_SOLVER_PARAMETERS
    acuPrep: Processing GRAVITY( 'none' )
    acuPrep: Processing GRAVITY( 'Gravity' )
    acuPrep: Processing ROTATION_FORCE( 'none' )
    acuPrep: Processing MASS_HEAT_SOURCE( 'none' )
    acuPrep: Processing MASS_HEAT_SOURCE( 'Gravity' )
    acuPrep: Processing VOLUME_HEAT_SOURCE( 'none' )
    acuPrep: Processing VOLUME_HEAT_SOURCE( 'Heatsource' )
    acuPrep: Processing MASS_SPECIES_SOURCE( 'none' )
    acuPrep: Processing VOLUME_SPECIES_SOURCE( 'none' )
    acuPrep: Processing BODY_FORCE( 'none' )
    acuPrep: Processing BODY_FORCE( 'Gravity' )
    acuPrep: Processing BODY_FORCE( 'Heatsource' )
    acuPrep: Processing DENSITY_MODEL( 'Air' )
    acuPrep: Processing DENSITY_MODEL( 'Aluminum' )
    acuPrep: Processing SPECIFIC_HEAT_MODEL( 'none' )
    acuPrep: Processing SPECIFIC_HEAT_MODEL( 'Air' )
    acuPrep: Processing SPECIFIC_HEAT_MODEL( 'Aluminum' )
    acuPrep: Processing VISCOSITY_MODEL( 'none' )
    acuPrep: Processing VISCOSITY_MODEL( 'Air' )
    acuPrep: Processing VISCOELASTIC_MODEL( 'none' )
    acuPrep: Processing CONDUCTIVITY_MODEL( 'none' )
    acuPrep: Processing CONDUCTIVITY_MODEL( 'Air' )
    acuPrep: Processing CONDUCTIVITY_MODEL( 'Aluminum' )
    acuPrep: Processing DIFFUSIVITY_MODEL( 'none' )
    acuPrep: Processing POROSITY_MODEL( 'none' )
    acuPrep: Processing POROSITY_MODEL( 'Air' )
    acuPrep: Processing MATERIAL_MODEL( 'Air' )
    acuPrep: Processing MATERIAL_MODEL( 'Aluminum' )
    acuPrep: Processing SURFACE_TENSION_MODEL( 'none' )
    acuPrep: Processing CONTACT_ANGLE_MODEL( 'none' )
    acuPrep: Processing EMISSIVITY_MODEL( 'none' )
    acuPrep: Processing SOLAR_RADIATION_MODEL( 'none' )
    acuPrep: Processing COORDINATE
    acuPrep: Processing NODAL_INITIAL_CONDITION( pressure )
    acuPrep: Processing NODAL_INITIAL_CONDITION( velocity )
    acuPrep: Processing NODAL_INITIAL_CONDITION( temperature )
    acuPrep: Processing NODAL_INITIAL_CONDITION( eddy_frequency )
    acuPrep: Processing NODAL_INITIAL_CONDITION( kinetic_energy )
    acuPrep: Processing NODAL_OUTPUT
    acuPrep: Processing DERIVED_QUANTITY_OUTPUT
    acuPrep: Processing RUNNING_AVERAGE_OUTPUT
    acuPrep: Processing TIME_AVERAGE_OUTPUT
    acuPrep: Processing RESTART_OUTPUT
    acuPrep: Processing ERROR_ESTIMATOR_OUTPUT
    acuPrep: Processing NODAL_RESIDUAL_OUTPUT
    acuPrep: Processing ELEMENT_SET( 'Fluid' )
    acuPrep: Processing ELEMENT_SET( 'solid' )
    acuPrep: Processing SIMPLE_BOUNDARY_CONDITION( 'Heatsource' )
    acuPrep: Processing SIMPLE_BOUNDARY_CONDITION( 'Outlet' )
    acuPrep: Processing SIMPLE_BOUNDARY_CONDITION( 'inlet' )
    acuPrep: Processing SIMPLE_BOUNDARY_CONDITION( 'wall' )
    acuPrep: Processing SURFACE_OUTPUT( 'Heatsource' )
    acuPrep: Processing SURFACE_OUTPUT( 'Outlet' )
    acuPrep: Processing SURFACE_OUTPUT( 'inlet' )
    acuPrep: Processing SURFACE_OUTPUT( 'wall' )
    acuPrep: Processing FWH_OUTPUT
    acuPrep: ------------------------------------------------------------------
    acuPrep:          Minimum coordinates = -1.9920e+002 5.4596e+002 5.0000e+000
    acuPrep:          Maximum coordinates = 3.4780e+002 1.0253e+003 1.5960e+002
    acuPrep:                  Total nodes =     255640
    acuPrep:               Total elements =    1222985
    acuPrep:                Element aggl. =          1
    acuPrep:    Total aggl. rad. surfaces =          0
    acuPrep:     Total interface surfaces =          0
    acuPrep: ------------------------------------------------------------------
    acuPrep:                  Output data = Subdomain 0
    acuPrep:                  Output data = Domain decomposition
    acuPrep:                  Output data = Surface output
    acuPrep: ------------------------------------------------------------------
    acuPrep:       Input  CPU/Elapse time = 1.100000e-001 1.250000e-001 Sec
    acuPrep:       Proc.  CPU/Elapse time = 2.371800e+001 2.421900e+001 Sec
    acuPrep:       Solar  CPU/Elapse time = 0.000000e+000 0.000000e+000 Sec
    acuPrep:       DDC    CPU/Elapse time = 2.500000e-001 2.650000e-001 Sec
    acuPrep:       Output CPU/Elapse time = 3.188000e+000 4.907000e+000 Sec
    acuPrep:       Total  CPU/Elapse time = 2.726600e+001 2.951600e+001 Sec
    acuPrep:            Total Memory Size = 6.574141e+002 Mbytes
    acuRun: -*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-
    acuRun: No enclosure radiation found: Bypassing acuView
    acuRun: -*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-*-
    acuRun: Run acuSolve ...
    acuRun: D:/Tools/Altair/12.0/acusolve/win64/bin/acuSolve.exe -np 1 -nt 1
    acuSolve: AcuSolve checked out license from HyperWorks
    acuSolve:                       Date = Mon Mar 24 16:45:08 2014
    acuSolve:                    Problem = CFD-sat
    acuSolve:                        Run = 9
    acuSolve:                      Title = ITA-1
    acuSolve:                   Subtitle = CFD
    acuSolve:                   Hostname = B2WS0468
    acuSolve:                   Platform = Whistler 5.2 unknown
    acuSolve:                    Machine = win64
    acuSolve:                    Release = 12.0.310
    acuSolve:               Release date = Aug 14 2013
    acuSolve:       Message passing type = none
    acuSolve:       Number of subdomains = 1
    acuSolve:       Number of processors = 1
    acuSolve:                  Non-zeros = 3418226
    acuSolve:          Working directory = ACUSIM.DIR
    acuSolve:
    acuSolve: ---------------------- Input Phase --------------------------
    acuSolve: Input CPU/Elapse time      = 4.874000e+000 6.188000e+000 Sec
    acuSolve: Input Memory Usage         = 1.075133e+003 Mbytes
    acuSolve: ---------------------- Begin Time Step ----------------------
    acuSolve: *** ASSERTION in Function <nbcSetTwf> File <nbc.c> Line <1275>
    acuSolve: *** Internal error
    acuRun: *** ERROR: error occurred executing acuSolve
    acuRun: Mon Mar 24 16:45:11 2014
     

  • Altair Forum User
    Altair Forum User
    Altair Employee
    edited March 2014

    Can u Tell me what kind off Error it may be!!?

  • Altair Forum User
    Altair Forum User
    Altair Employee
    edited March 2014

    I am Using 12.0.310 Acusolve version!!!

  • Altair Forum User
    Altair Forum User
    Altair Employee
    edited March 2014

    # DATE: Mon Mar 24 15:01:17 2014
    # VERSION: 12.0.310
    #1# INCLUDE 'dinesh_3.rst'
    ANALYSIS {
        title = 'TITLE' ;
        sub_title = 'SUBTITLE' ;
        input_version = 'unknown' ;
        type = static ;
    }
    EQUATION {
        flow = navier_stokes ;
        absolute_pressure_offset = 101325 ;
        temperature = advective_diffusive ;
        absolute_temperature_offset = 273 ;
        radiation = none ;
        species_transport = none ;
        turbulence = k_omega ;
        mesh = eulerian ;
        particle_trace = off ;
        external_code = off ;
        running_average = off ;
    }
    AUTO_SOLUTION_STRATEGY {
        max_time_steps = 300 ;
        initial_time_increment = 0.1 ;
        convergence_tolerance = 0.001 ;
        num_krylov_vectors = 40 ;
        flow = on ;
        temperature = on ;
        temperature_flow = on ;
        relaxation_factor = 0.25 ;
    }
    #2# INCLUDE 'demo.ss.inc'
    TIME_SEQUENCE {
        final_time = 0 ;
        min_time_steps = 1 ;
        max_time_steps = 300 ;
        convergence_tolerance = 0.001 ;
        termination_delay = 0 ;
        lhs_update_initial_times = 1 ;
        lhs_update_frequency = 1 ;
        min_stagger_iterations = 1 ;
        max_stagger_iterations = 1 ;
        stagger_convergence_tolerance = 1 ;
        stagger_lhs_update_frequency = 1 ;
        staggers = { 'temperature_flow',
                     'eddy_frequency',
                     'kinetic_energy' } ;
    }
    STAGGER( 'temperature_flow' ) {
        equation = temperature_flow ;
        min_stagger_iterations = 1 ;
        max_stagger_iterations = 1 ;
        convergence_tolerance = 0.1 ;
        lhs_update_frequency = 1 ;
        linear_solver = gmres ;
        min_linear_solver_iterations = 10 ;
        max_linear_solver_iterations = 1000 ;
        num_krylov_vectors = 40 ;
        linear_solver_tolerance = 0.1 ;
        pressure_projection_tolerance = 0.01 ;
        temperature_projection_tolerance = 0.001 ;
        projection = off ;
        pressure_projection = on ;
        temperature_projection = on ;
        pressure_algebraic_multigrid = off ;
    }
    STAGGER( 'eddy_frequency' ) {
        equation = eddy_frequency ;
        min_stagger_iterations = 1 ;
        max_stagger_iterations = 1 ;
        convergence_tolerance = 0.1 ;
        lhs_update_frequency = 1 ;
        linear_solver = gmres ;
        min_linear_solver_iterations = 10 ;
        max_linear_solver_iterations = 1000 ;
        num_krylov_vectors = 100 ;
        linear_solver_tolerance = 0.001 ;
        projection = off ;
    }
    STAGGER( 'kinetic_energy' ) {
        equation = kinetic_energy ;
        min_stagger_iterations = 1 ;
        max_stagger_iterations = 1 ;
        convergence_tolerance = 0.1 ;
        lhs_update_frequency = 1 ;
        linear_solver = gmres ;
        min_linear_solver_iterations = 10 ;
        max_linear_solver_iterations = 1000 ;
        num_krylov_vectors = 100 ;
        linear_solver_tolerance = 0.01 ;
        projection = off ;
    }
    TIME_INCREMENT {
        initial_time_increment = 0.1 ;
        auto_time_increment = off ;
        local_time_increment = off ;
        min_time_increment = 0 ;
        max_time_increment = 0 ;
        cfl_control = off ;
        cfl_number = 1000 ;
        min_cfl_number = 0 ;
        initial_cfl_number = 1 ;
        time_increment_decrease_factor = 0.25 ;
        time_increment_increase_factor = 1.25 ;
        time_increment_increase_delay = 4 ;
        min_time_increment_ratio = 0.1 ;
        multiplier_function = 'none' ;
    }
    TIME_INTEGRATION {
        predictor = same_v ;
        time_integration_order = first ;
        high_frequency_damping_factor = 1 ;
        pressure_damping_type = max ;
        lumped_mass_factor = 1 ;
        initialize_acceleration = off ;
    }
    LINEAR_SOLVER_PARAMETERS {
        lhs_storage = reduced_memory_sparse ;
        min_num_iteration_ratio = 0.5 ;
        pressure_precedence_factor = 1 ;
        num_pressure_projection_vectors = 10 ;
        num_velocity_projection_vectors = 5 ;
        num_flow_projection_vectors = 5 ;
        num_viscoelastic_stress_projection_vectors = 5 ;
        num_temperature_projection_vectors = 10 ;
        num_radiation_projection_vectors = 10 ;
        num_temperature_flow_projection_vectors = 4 ;
        num_species_projection_vectors = 10 ;
        num_turbulence_projection_vectors = 10 ;
        num_mesh_displacement_projection_vectors = 10 ;
        pressure_lhs_inverse_order = 5 ;
        velocity_lhs_inverse_order = 5 ;
        flow_lhs_inverse_order = 5 ;
        temperature_lhs_inverse_order = 6 ;
        pressure_regularization_factor = 1 ;
        velocity_regularization_factor = 0.5 ;
        flow_regularization_factor = 0 ;
        viscoelastic_stress_regularization_factor = 0 ;
        temperature_regularization_factor = 0 ;
        temperature_flow_regularization_factor = 0 ;
        species_regularization_factor = 0 ;
        turbulence_regularization_factor = 0 ;
        mesh_displacement_regularization_factor = 0 ;
        pressure_update_factor = 1 ;
        velocity_update_factor = 0.75 ;
        viscoelastic_stress_update_factor = 0.75 ;
        temperature_update_factor = 1 ;
        species_update_factor = 1 ;
        turbulence_update_factor = 0.75 ;
        mesh_displacement_update_factor = 1 ;
        radiation_update_factor = 1 ;
        max_pressure_update = 0 ;
        max_velocity_update = 0 ;
        max_viscoelastic_stress_update = 0 ;
        max_temperature_update = 0 ;
        max_species_update = 0 ;
        max_turbulence_update = 0 ;
        max_mesh_displacement_update = 0 ;
        max_radiation_update = 0 ;
        max_reverse_update_factor = 0 ;
    }
    CONVERGENCE_CHECK_PARAMETERS {
        pressure_residual_check = standard ;
        pressure_solution_increment_check = looser_by_10 ;
        velocity_residual_check = standard ;
        velocity_solution_increment_check = looser_by_10 ;
        viscoelastic_stress_residual_check = looser_by_10 ;
        viscoelastic_stress_solution_increment_check = looser_by_10 ;
        temperature_residual_check = standard ;
        temperature_solution_increment_check = looser_by_10 ;
        radiation_residual_check = none ;
        radiation_solution_increment_check = looser_by_10 ;
        species_residual_check = standard ;
        species_solution_increment_check = looser_by_10 ;
        turbulence_residual_check = looser_by_10 ;
        turbulence_solution_increment_check = looser_by_100 ;
        mesh_displacement_residual_check = none ;
        mesh_displacement_solution_increment_check = looser_by_100 ;
    }
    ALGEBRAIC_MULTIGRID_PARAMETERS {
        pressure_standard_interpolation = on ;
        pressure_truncated_interpolation = on ;
        pressure_negative_coupling_tolerance = 0.25 ;
        pressure_positive_coupling_tolerance = 0.5 ;
        pressure_truncation_tolerance = 0.2 ;
        max_pressure_final_matrix = 100 ;
        pressure_eigenvalue_tolerance = 1e-006 ;
        max_pressure_eigenvalue_iterations = 100 ;
        pressure_smoothing_order = 2 ;
        pressure_chebyshev_max_min_ratio = 10 ;
        num_pressure_global_basis = 0 ;
        pressure_global_basis_tolerance = 1e-006 ;
        max_pressure_global_basis_iterations = 1000 ;
        num_pressure_initial_givens_rotations = 0 ;
    }
    MATERIAL_MODEL( 'Air' ) {
        type = fluid ;
        density_model = 'Air' ;
        specific_heat_model = 'Air' ;
        viscosity_model = 'Air' ;
        conductivity_model = 'Air' ;
        porosity_model = 'Air' ;
    }
    #2# END INCLUDE 'demo.ss.inc'
    DENSITY_MODEL( 'Air' ) {
        type = constant ;
        density = 1.225 ;
        isothermal_compressibility = 0 ;
    }
    VISCOSITY_MODEL( 'Air' ) {
        type = constant ;
        viscosity = 1.781e-005 ;
    }
    SPECIFIC_HEAT_MODEL( 'Air' ) {
        type = constant ;
        specific_heat = 1005 ;
        latent_heat_type = none ;
    }
    CONDUCTIVITY_MODEL( 'Air' ) {
        type = constant ;
        conductivity = 0.02521 ;
        turbulent_prandtl_number = 0.91 ;
    }
    POROSITY_MODEL( 'Air' ) {
        type = none ;
    }
    MATERIAL_MODEL( 'Aluminum' ) {
        type = solid ;
        density_model = 'Aluminum' ;
        specific_heat_model = 'Aluminum' ;
        conductivity_model = 'Aluminum' ;
    }
    DENSITY_MODEL( 'Aluminum' ) {
        type = constant ;
        density = 2710 ;
        isothermal_compressibility = 0 ;
    }
    SPECIFIC_HEAT_MODEL( 'Aluminum' ) {
        type = constant ;
        specific_heat = 963 ;
        latent_heat_type = none ;
    }
    CONDUCTIVITY_MODEL( 'Aluminum' ) {
        type = constant ;
        conductivity = 113 ;
    }
    BODY_FORCE( 'Gravity' ) {
        gravity = 'Gravity' ;
        mass_heat_source = 'Gravity' ;
    }
    GRAVITY( 'Gravity' ) {
        type = constant ;
        gravity = { 0, 0, -9.810000000000001; } ;
    }
    MASS_HEAT_SOURCE( 'Gravity' ) {
        type = constant ;
        mass_heat_source = 0 ;
    }
    BODY_FORCE( 'Heat Source' ) {
        volume_heat_source = 'Heat Source' ;
    }
    VOLUME_HEAT_SOURCE( 'Heat Source' ) {
        type = constant ;
        volume_heat_source = 635000 ;
    }
    FWH_OUTPUT {
        reference_density = 1.225 ;
        reference_pressure = 0 ;
        reference_sound_speed = 330 ;
        source_output_frequency = 0 ;
        source_output_time_interval = 0 ;
        num_source_saved_states = 0 ;
    }
    NODAL_OUTPUT {
        output_frequency = 10 ;
        output_time_interval = 0 ;
        output_initial_condition = off ;
        continuous_output = off ;
        num_saved_states = 0 ;
    }
    DERIVED_QUANTITY_OUTPUT {
        output_frequency = 10 ;
        output_time_interval = 0 ;
        num_saved_states = 0 ;
    }
    RUNNING_AVERAGE_OUTPUT {
        output_frequency = 1000 ;
        output_time_interval = 0 ;
        num_saved_states = 0 ;
    }
    TIME_AVERAGE_OUTPUT {
        order = 2 ;
        output_frequency = 0 ;
        output_time_interval = 0 ;
        reset_frequency = 0 ;
        num_saved_states = 0 ;
    }
    ERROR_ESTIMATOR_OUTPUT {
        type = pde_residual ;
        output_frequency = 0 ;
        output_time_interval = 0 ;
        num_saved_states = 0 ;
        time_average_output_frequency = 0 ;
        time_average_output_time_interval = 0 ;
        num_time_average_saved_states = 0 ;
        time_average_reset_frequency = 0 ;
    }
    RESTART_OUTPUT {
        output_frequency = 100 ;
        output_time_interval = 0 ;
        num_saved_states = 2 ;
    }
    NODAL_RESIDUAL_OUTPUT {
        output_frequency = 0 ;
        output_time_interval = 0 ;
        num_saved_states = 0 ;
    }
    NODAL_INITIAL_CONDITION( pressure ) {
        default_value = 101325 ;
        satisfy_boundary_condition = off ;
    }
    NODAL_INITIAL_CONDITION( velocity ) {
        default_values = { 0, 0, 0; } ;
        satisfy_boundary_condition = off ;
    }
    NODAL_INITIAL_CONDITION( temperature ) {
        default_value = 298 ;
        satisfy_boundary_condition = off ;
    }
    NODAL_INITIAL_CONDITION( eddy_frequency ) {
        default_value = 0 ;
        satisfy_boundary_condition = off ;
    }
    NODAL_INITIAL_CONDITION( kinetic_energy ) {
        default_value = 0 ;
        satisfy_boundary_condition = off ;
    }
    COORDINATE {
        coordinates = Read( 'MESH.DIR/dinesh_3.crd' ) ;
    }
    ELEMENT_SET( 'Fluid' ) {
        shape = four_node_tet ;
        elements = Read( 'MESH.DIR/dinesh_3.Fluid.tet4.cnn' ) ;
        medium = fluid ;
        quadrature = full ;
        material_model = 'Air' ;
        body_force = 'Gravity' ;
        reference_frame = 'none' ;
        mesh_motion = 'none' ;
        viscous_heating = off ;
        compression_heating = off ;
        residual_control = on ;
        oscillation_control = on ;
    }
    ELEMENT_SET( 'Solid' ) {
        shape = four_node_tet ;
        elements = Read( 'MESH.DIR/dinesh_3.Solid.tet4.cnn' ) ;
        medium = solid ;
        quadrature = full ;
        material_model = 'Aluminum' ;
        body_force = 'none' ;
        element_volume_heat_sources = Read( 'MESH.DIR/dinesh_3.Solid.tet4.vhs' ) ;
        mesh_motion = 'none' ;
    }
    SIMPLE_BOUNDARY_CONDITION( 'Inlet' ) {
        shape = three_node_triangle ;
        element_set = 'Fluid' ;
        surfaces = Read( 'MESH.DIR/dinesh_3.Fluid.tet4.Inlet.tri3.ebc' ) ;
        type = inflow ;
        inflow_type = pressure ;
        precedence = 1 ;
        reference_frame = 'none' ;
        pressure = 0 ;
        pressure_loss_factor = 0 ;
        hydrostatic_pressure = off ;
        temperature = 298 ;
        kinetic_energy = 0.00135 ;
        eddy_frequency = 0.067082039325 ;
        non_reflecting_factor = 0 ;
        active_type = all ;
    }
    SURFACE_OUTPUT( 'Inlet' ) {
        shape = three_node_triangle ;
        element_set = 'Fluid' ;
        surfaces = Read( 'MESH.DIR/dinesh_3.Fluid.tet4.Inlet.tri3.ebc' ) ;
        integrated_output_frequency = 1 ;
        integrated_output_time_interval = 0 ;
        statistics_output_frequency = 1 ;
        statistics_output_time_interval = 0 ;
        nodal_output_frequency = 0 ;
        nodal_output_time_interval = 0 ;
        num_saved_states = 0 ;
    }
    SIMPLE_BOUNDARY_CONDITION( 'Source' ) {
        shape = three_node_triangle ;
        element_set = 'Fluid' ;
        surfaces = Read( 'MESH.DIR/dinesh_3.Fluid.tet4.Source.tri3.ebc' ) ;
        type = wall ;
        precedence = 1 ;
        reference_frame = 'none' ;
        wall_velocity_type = match_mesh_velocity ;
        temperature_type = flux ;
        heat_flux = 0 ;
        convective_heat_coefficient = 1.5 ;
        convective_heat_reference_temperature = 298 ;
        turbulence_wall_type = wall_function ;
        roughness_height = 0 ;
        active_type = all ;
    }
    SURFACE_OUTPUT( 'Source' ) {
        shape = three_node_triangle ;
        element_set = 'Fluid' ;
        surfaces = Read( 'MESH.DIR/dinesh_3.Fluid.tet4.Source.tri3.ebc' ) ;
        integrated_output_frequency = 1 ;
        integrated_output_time_interval = 0 ;
        statistics_output_frequency = 1 ;
        statistics_output_time_interval = 0 ;
        nodal_output_frequency = 0 ;
        nodal_output_time_interval = 0 ;
        num_saved_states = 0 ;
    }
    SIMPLE_BOUNDARY_CONDITION( 'outlet' ) {
        shape = three_node_triangle ;
        element_set = 'Fluid' ;
        surfaces = Read( 'MESH.DIR/dinesh_3.Fluid.tet4.outlet.tri3.ebc' ) ;
        type = outflow ;
        precedence = 1 ;
        pressure = 0 ;
        pressure_loss_factor = 0 ;
        hydrostatic_pressure = off ;
        non_reflecting_factor = 0 ;
        active_type = all ;
    }
    SURFACE_OUTPUT( 'outlet' ) {
        shape = three_node_triangle ;
        element_set = 'Fluid' ;
        surfaces = Read( 'MESH.DIR/dinesh_3.Fluid.tet4.outlet.tri3.ebc' ) ;
        integrated_output_frequency = 1 ;
        integrated_output_time_interval = 0 ;
        statistics_output_frequency = 1 ;
        statistics_output_time_interval = 0 ;
        nodal_output_frequency = 0 ;
        nodal_output_time_interval = 0 ;
        num_saved_states = 0 ;
    }
    SIMPLE_BOUNDARY_CONDITION( 'wall' ) {
        shape = three_node_triangle ;
        element_set = 'Fluid' ;
        surfaces = Read( 'MESH.DIR/dinesh_3.Fluid.tet4.wall.tri3.ebc' ) ;
        type = wall ;
        precedence = 1 ;
        reference_frame = 'none' ;
        wall_velocity_type = match_mesh_velocity ;
        temperature_type = value ;
        temperature = 298 ;
        turbulence_wall_type = none ;
        active_type = all ;
    }
    SURFACE_OUTPUT( 'wall' ) {
        shape = three_node_triangle ;
        element_set = 'Fluid' ;
        surfaces = Read( 'MESH.DIR/dinesh_3.Fluid.tet4.wall.tri3.ebc' ) ;
        integrated_output_frequency = 1 ;
        integrated_output_time_interval = 0 ;
        statistics_output_frequency = 1 ;
        statistics_output_time_interval = 0 ;
        nodal_output_frequency = 0 ;
        nodal_output_time_interval = 0 ;
        num_saved_states = 0 ;
    }
    RESTART {
        type = full ;
        from_problem = 'dinesh' ;
        from_directory = 'ACUSIM.DIR' ;
        from_run = 2 ;
        from_time_step = 3 ;
        reset_time_step = off ;
        reset_time_increment = off ;
    }
    RUN
     

  • cfdguru
    cfdguru New Altair Community Member
    edited March 2014

    Do you still see the error if you set the turbulence model to Spalart-Allmaras?

  • Altair Forum User
    Altair Forum User
    Altair Employee
    edited May 2014

    yeah when i Change Model from spalart allmaras to K omega I am getting same error

  • Filip Klouda
    Filip Klouda New Altair Community Member
    edited August 2019

    Hello,

     

    I think K omega can be used only for steady state analysis.

     

    Filip