TURBIGEN v1.10.1
Starting at 2025-01-03T09:18:11
Working directory: /home/jb753/python/turbigen-dev/doc/runs/cascade_test
Inlet: PerfectState(P=1.000 bar, T=300.0 K)
Designing a turbine_cascade mean line...
MeanLine(
    Po=[1.    0.975] bar,
    To=[300. 300.] K,
    Ma=[0.336 0.6  ],
    Vx=[88.4 85.1],
    Vr=[0. 0.],
    Vt=[  74.2 -182.4],
    Vt_rel=[  74.2 -182.4],
    Al=[ 40. -65.],
    Al_rel=[ 40. -65.],
    rpm=[0. 0.],
    mdot=[57.95 57.95] kg/s
    )
Checking mean-line conservation...
Checking mean-line inversion...
Designing annulus...
Error encountered, quitting...
Traceback (most recent call last):
  File "/home/jb753/.pyenv/versions/turbigen-dev/bin/turbigen", line 8, in <module>
    sys.exit(main())
             ^^^^^^
  File "/home/jb753/python/turbigen-dev/turbigen/main.py", line 259, in main
    success = turbigen.run.run(conf)
              ^^^^^^^^^^^^^^^^^^^^^^
  File "/home/jb753/python/turbigen-dev/turbigen/run.py", line 1333, in run
    ml_out, _, gguess = run_single(conf)
                        ^^^^^^^^^^^^^^^^
  File "/home/jb753/python/turbigen-dev/turbigen/run.py", line 180, in run_single
    ann = Annulus(ml.rmid, ml.span, ml.Beta, **conf.annulus)
          ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
TypeError: Smooth.__init__() got an unexpected keyword argument 'debug'
TURBIGEN v1.10.1
Starting at 2025-01-03T09:19:07
Working directory: /home/jb753/python/turbigen-dev/doc/runs/cascade_test
Inlet: PerfectState(P=1.000 bar, T=300.0 K)
Designing a turbine_cascade mean line...
MeanLine(
    Po=[1.    0.975] bar,
    To=[300. 300.] K,
    Ma=[0.336 0.6  ],
    Vx=[88.4 85.1],
    Vr=[0. 0.],
    Vt=[  74.2 -182.4],
    Vt_rel=[  74.2 -182.4],
    Al=[ 40. -65.],
    Al_rel=[ 40. -65.],
    rpm=[0. 0.],
    mdot=[57.95 57.95] kg/s
    )
Checking mean-line conservation...
Checking mean-line inversion...
Designing annulus...
Annulus(
    xmid=[-1.4868e-12  6.8784e-02],
    rmid=[0.95 0.95],
    span=[0.1  0.12]
    )
Re_surf/10^5=[11.6]
Nblade=[99], s_cm=[0.88], tip=[0.]
Generating an H-mesh...
Mesh Npts/10^6=1.57
Applying boundary conditions...
Setting intial guess...
Calculating wall distance...
No solver specified, continuing with initial guess...
Post-processing...
Mixed-out CFD result:
MeanLine(
    Po=[1.     0.9748] bar,
    To=[300. 300.] K,
    Ma=[0.336 0.6  ],
    Vx=[88.4 85.1],
    Vr=[0. 0.],
    Vt=[  74.2 -182.3],
    Vt_rel=[  74.2 -182.3],
    Al=[ 39.99 -64.98],
    Al_rel=[ 39.99 -64.98],
    rpm=[0. 0.],
    mdot=[57.95 57.95] kg/s
    )
Design variable Nom    CFD    
------------------------------
Alpha           [40.0, [ 39.9 
Ma2             0.6000 0.5996 
Yh              0.1000 0.1010 
htr             0.9000 0.9000 
span            [0.1,  [0.1   
eta_tt=0.000, eta_ts=0.000
Elapsed time 0.36 min.
