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Aeroelastics Lab, Aeronautics Department.
    Copyright (c), Imperial College London.
    All rights reserved. 
    License available at https://github.com/imperialcollegelondon/sharpy
Running SHARPy from /home/ng213/code/sharpy/tests
SHARPy being run is in /home/ng213/code/sharpy
The branch being run is temp_dev
The version and commit hash are: v0.1-1429-g332be7d-332be7d
The available solvers on this session are:
Cleanup 
FrequencyResponse 
PickleData 
SaveData 
CreateSnapshot 
PlotFlowField 
StabilityDerivatives 
AeroForcesCalculator 
WriteVariablesTime 
AerogridPlot 
LiftDistribution 
StallCheck 
_BaseStructural 
AerogridLoader 
BeamLoader 
DynamicCoupled 
DynamicUVLM 
LinDynamicSim 
LinearAssembler 
Modal 
NoAero 
NonLinearDynamic 
NonLinearDynamicCoupledStep 
NonLinearDynamicMultibody 
NonLinearDynamicPrescribedStep 
NonLinearStatic 
NonLinearStaticMultibody 
PrescribedUvlm 
RigidDynamicPrescribedStep 
SHWUvlm 
StaticCoupled 
StaticCoupledRBM 
StaticTrim 
StaticUvlm 
StepLinearUVLM 
StepUvlm 
Trim 
AsymptoticStability 
BeamPlot 
BeamLoads 
PreSharpy 
Generating an instance of BeamLoader
Generating an instance of AerogridLoader
The aerodynamic grid contains 3 surfaces
  Surface 0, M=4, N=46
     Wake 0, M=1, N=46
  Surface 1, M=4, N=46
     Wake 1, M=1, N=46
  Surface 2, M=4, N=46
     Wake 2, M=1, N=46
  In total: 552 bound panels
  In total: 138 wake panels
  Total number of panels = 690
Generating an instance of StaticCoupledRBM
Generating an instance of RigidDynamicPrescribedStep
Generating an instance of SHWUvlm
i_step: 0, i_iter: 0
i_step: 0, i_iter: 1
Pos res     = 0.000000e+00. Psi res     = 0.000000e+00.
Pos_dot res = 0.000000e+00. Psi_dot res = 0.000000e+00.
Resultant forces and moments: (array([8.876893877069847e-02, 1.113122280350467e-01, 6.617098446408015e+05]), array([-3.619568084104685e-03, -4.279360481268668e-02,  4.279531346799329e+06]))
Generating an instance of DynamicCoupled
Generating an instance of RigidDynamicPrescribedStep
Generating an instance of StepUvlm
Generating an instance of BeamPlot
Generating an instance of AerogridPlot
Generating an instance of Cleanup
Generating an instance of SaveData
Variable save_linear has no assigned value in the settings file.
    will default to the value: c_bool(False)
Variable save_linear_uvlm has no assigned value in the settings file.
    will default to the value: c_bool(False)
Variable skip_attr has no assigned value in the settings file.
    will default to the value: ['fortran', 'airfoils', 'airfoil_db', 'settings_types', 'ct_dynamic_forces_list', 'ct_gamma_dot_list', 'ct_gamma_list', 'ct_gamma_star_list', 'ct_normals_list', 'ct_u_ext_list', 'ct_u_ext_star_list', 'ct_zeta_dot_list', 'ct_zeta_list', 'ct_zeta_star_list', 'dynamic_input', ['fortran', 'airfoils', 'airfoil_db', 'settings_types', 'ct_dynamic_forces_list', 'ct_forces_list', 'ct_gamma_dot_list', 'ct_gamma_list', 'ct_gamma_star_list', 'ct_normals_list', 'ct_u_ext_list', 'ct_u_ext_star_list', 'ct_zeta_dot_list', 'ct_zeta_list', 'ct_zeta_star_list', 'dynamic_input']]
Variable format has no assigned value in the settings file.
    will default to the value: h5



|=======|========|======|==============|==============|==============|==============|==============|
|  ts   |   t    | iter | struc ratio  |  iter time   | residual vel |  FoR_vel(x)  |  FoR_vel(z)  |
|=======|========|======|==============|==============|==============|==============|==============|
|   1   | 0.0511 |  1   |   0.068213   |   0.743148   |     -inf     | 0.000000e+00 | 0.000000e+00 |
...Finished
Generating an instance of SaveData
Variable save_linear has no assigned value in the settings file.
    will default to the value: c_bool(False)
Variable save_linear_uvlm has no assigned value in the settings file.
    will default to the value: c_bool(False)
Variable skip_attr has no assigned value in the settings file.
    will default to the value: ['fortran', 'airfoils', 'airfoil_db', 'settings_types', 'ct_dynamic_forces_list', 'ct_gamma_dot_list', 'ct_gamma_list', 'ct_gamma_star_list', 'ct_normals_list', 'ct_u_ext_list', 'ct_u_ext_star_list', 'ct_zeta_dot_list', 'ct_zeta_list', 'ct_zeta_star_list', 'dynamic_input', ['fortran', 'airfoils', 'airfoil_db', 'settings_types', 'ct_dynamic_forces_list', 'ct_forces_list', 'ct_gamma_dot_list', 'ct_gamma_list', 'ct_gamma_star_list', 'ct_normals_list', 'ct_u_ext_list', 'ct_u_ext_star_list', 'ct_zeta_dot_list', 'ct_zeta_list', 'ct_zeta_star_list', 'dynamic_input'], ['fortran', 'airfoils', 'airfoil_db', 'settings_types', 'ct_dynamic_forces_list', 'ct_forces_list', 'ct_gamma_dot_list', 'ct_gamma_list', 'ct_gamma_star_list', 'ct_normals_list', 'ct_u_ext_list', 'ct_u_ext_star_list', 'ct_zeta_dot_list', 'ct_zeta_list', 'ct_zeta_star_list', 'dynamic_input']]
Variable format has no assigned value in the settings file.
    will default to the value: h5
FINISHED - Elapsed time = 2.3944626 seconds
FINISHED - CPU process time = 2.3888776 seconds
