TURBIGEN v1.5.1
Starting at 2024-01-05T09:59:36
Working directory: /home/jb753/python/turbigen-open/doc/runs/cascade
Inlet: PerfectState(P=1.000 bar, T=300.0 K)
Designing a cascade...
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...
Annulus(
    xmid=[-3.8624e-12  6.8750e-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=0.86
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=[-2.5e-13  0.0e+00],
    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
    )
eta_tt=0.000, eta_ts=0.000
Design variable Nom    CFD    
------------------------------
Alpha1          40.000 39.986 
Alpha2          -65.00 -64.98 
Ma2             0.6000 0.5996 
Yh              0.1000 0.1010 
htr             0.9000 0.9000 
span1           0.1000 0.1000 
span2           0.1200 0.1200 
Elapsed time 0.20 min.
TURBIGEN v1.5.1
Starting at 2024-02-02T15:37:36
Working directory: /home/jb753/python/turbigen-open/doc/runs/cascade
Inlet: PerfectState(P=1.000 bar, T=300.0 K)
Designing a cascade...
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...
Annulus(
    xmid=[-3.7438e-12  6.8750e-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=[-2.6e-13  0.0e+00],
    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    
------------------------------
Alpha1          40.000 39.986 
Alpha2          -65.00 -64.98 
Ma2             0.6000 0.5996 
Yh              0.1000 0.1010 
htr             0.9000 0.9000 
span1           0.1000 0.1000 
span2           0.1200 0.1200 
eta_tt=0.000, eta_ts=0.000
Elapsed time 0.17 min.
