TURBIGEN v1.9.1
Starting at 2025-01-24T16:29:47
Working directory: /rds/project/rds-7OSWtyyYICQ/jb753/turbigen-dev/tests/back-to-back/compressor/ts3
Inlet: PerfectState(P=1.000 bar, T=300.0 K)
Designing a axial_compressor_rotor mean line...
MeanLine(
    Po=[1.  1.1] bar,
    To=[300.     308.8103] K,
    Ma=[0.259 0.307],
    Vx=[89.3 89.3],
    Vr=[0. 0.],
    Vt=[ 0.  59.5],
    Vt_rel=[-148.8  -89.3],
    Al=[ 0.   33.69],
    Al_rel=[-59.04 -45.  ],
    rpm=[7471. 7471.],
    mdot=[5. 5.] kg/s
    )
Checking mean-line conservation...
Checking mean-line inversion...
Designing annulus...
Annulus(
    xmid=[2.3276e-10 2.0464e-02],
    rmid=[0.189  0.1891],
    span=[0.042  0.0398]
    )
Re_surf/10^5=[3.4]
Nblade=[34], s_cm=[1.71], tip=[0.]
Generating OH-mesh...
Making a new mesh.
Error encountered, quitting...
Traceback (most recent call last):
  File "/home/jb753/rds/rds-gp10006-pullan-mhi/jb753/pyenv/versions/turbigen-dev/bin/turbigen", line 8, in <module>
    sys.exit(main())
             ^^^^^^
  File "/rds/project/gp10006/rds-gp10006-pullan-mhi/jb753/turbigen-dev/turbigen/main.py", line 259, in main
    success = turbigen.run.run(conf)
              ^^^^^^^^^^^^^^^^^^^^^^
  File "/rds/project/gp10006/rds-gp10006-pullan-mhi/jb753/turbigen-dev/turbigen/run.py", line 1350, in run
    ml_out, _, gguess = run_single(conf)
                        ^^^^^^^^^^^^^^^^
  File "/rds/project/gp10006/rds-gp10006-pullan-mhi/jb753/turbigen-dev/turbigen/run.py", line 741, in run_single
    g = ohmesh.make_grid(mac, ohmesh_config, dhub, dcas, drow, unbladed, Omega)
        ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/rds/project/gp10006/rds-gp10006-pullan-mhi/jb753/turbigen-dev/turbigen/ohmesh.py", line 234, in make_grid
    success = turbigen.autogrid.autogrid.make_mesh(
              ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/rds/project/gp10006/rds-gp10006-pullan-mhi/jb753/turbigen-dev/turbigen/autogrid/autogrid.py", line 579, in make_mesh
    success = _run_remote(
              ^^^^^^^^^^^^
  File "/rds/project/gp10006/rds-gp10006-pullan-mhi/jb753/turbigen-dev/turbigen/autogrid/autogrid.py", line 402, in _run_remote
    _execute_on_remote(
  File "/rds/project/gp10006/rds-gp10006-pullan-mhi/jb753/turbigen-dev/turbigen/autogrid/autogrid.py", line 336, in _execute_on_remote
    out = subprocess.check_output(
          ^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jb753/rds/rds-gp10006-pullan-mhi/jb753/pyenv/versions/3.11.9/lib/python3.11/subprocess.py", line 466, in check_output
    return run(*popenargs, stdout=PIPE, timeout=timeout, check=True,
           ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jb753/rds/rds-gp10006-pullan-mhi/jb753/pyenv/versions/3.11.9/lib/python3.11/subprocess.py", line 550, in run
    stdout, stderr = process.communicate(input, timeout=timeout)
                     ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jb753/rds/rds-gp10006-pullan-mhi/jb753/pyenv/versions/3.11.9/lib/python3.11/subprocess.py", line 1209, in communicate
    stdout, stderr = self._communicate(input, endtime, timeout)
                     ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jb753/rds/rds-gp10006-pullan-mhi/jb753/pyenv/versions/3.11.9/lib/python3.11/subprocess.py", line 2115, in _communicate
    ready = selector.select(timeout)
            ^^^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jb753/rds/rds-gp10006-pullan-mhi/jb753/pyenv/versions/3.11.9/lib/python3.11/selectors.py", line 415, in select
    fd_event_list = self._selector.poll(timeout)
                    ^^^^^^^^^^^^^^^^^^^^^^^^^^^^
KeyboardInterrupt
TURBIGEN v1.9.1
Starting at 2025-01-24T16:30:50
Working directory: /rds/project/rds-7OSWtyyYICQ/jb753/turbigen-dev/tests/back-to-back/compressor/ts3
Inlet: PerfectState(P=1.000 bar, T=300.0 K)
Designing a axial_compressor_rotor mean line...
MeanLine(
    Po=[1.  1.1] bar,
    To=[300.     308.8103] K,
    Ma=[0.259 0.307],
    Vx=[89.3 89.3],
    Vr=[0. 0.],
    Vt=[ 0.  59.5],
    Vt_rel=[-148.8  -89.3],
    Al=[ 0.   33.69],
    Al_rel=[-59.04 -45.  ],
    rpm=[7471. 7471.],
    mdot=[5. 5.] kg/s
    )
Checking mean-line conservation...
Checking mean-line inversion...
Designing annulus...
Annulus(
    xmid=[2.3276e-10 2.0464e-02],
    rmid=[0.189  0.1891],
    span=[0.042  0.0398]
    )
Re_surf/10^5=[3.4]
Nblade=[34], s_cm=[1.71], tip=[0.]
Generating OH-mesh...
Making a new mesh.
Mesh Npts/10^6=0.36
Applying boundary conditions...
Running off-design: setting total-static pressure ratio PR_ts=1.0
Setting intial guess...
Calculating wall distance...
Running solver ts3...
Using 1 GPUs on 1 nodes, 1 per node.
Post-processing...
Contouring...
Plotting convergence...
Plotting pressure distributions, row 0 at spf=[0.5]
Mixed-out CFD result:
MeanLine(
    Po=[0.999  1.0868] bar,
    To=[300.2009 307.9633] K,
    Ma=[0.268 0.308],
    Vx=[92.3 92.8],
    Vr=[1.9 0.2],
    Vt=[ 1.4 53.7],
    Vt_rel=[-147.4  -95.1],
    Al=[ 0.84 30.07],
    Al_rel=[-57.94 -45.69],
    rpm=[7471. 7471.],
    mdot=[5.15 5.15] kg/s
    )
Design variable Nom    CFD    
------------------------------
PR              1.1000 1.0879 
etatt           0.9400 0.9422 
htr1            0.8000 0.8000 
mdot            5.0000 5.1515 
phi             0.6000 0.6205 
psi             0.4000 0.3524 
eta_tt=0.942, eta_ts=0.207
Elapsed time 4.41 min.
