[kh3]

When I try this tutorial: Unconstrained shape design of a transonic inviscid airfoil at a cte. AoA. I download everything they required python, su2, NumPy, and SciPy. And also, I had performed the SU2_CFD, SU2_DOT, SU2_GEO and SU2_DEF to get all the file I needed.But when I run this two line the error occur----> raise exception(message)
SU2.EvaluationFailure: Path = D:\SU2\Naopt\DESIGNS\DSN_001\DIRECT\,
Command = "D:\bin\SU2_CFD" config_CFD.cfg
SU2 process returned error '1'
The system cannot find the path specified.


I did not create the DIRECT file this file appear after I run the below command lines.

///////////
PS C:\Windows\System32\WindowsPowerShell\v1.0> cd D:\SU2\Naopt\

PS D:\SU2\Naopt> D:\SU2-v8.0.0-win64\bin\shape_optimization.py -g CONTINUOUS_ADJOINT -o SLSQP -f inv_NACA0012_basic.cfg

-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Aerodynamic Shape Optimization Script |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors (cf. AUTHORS.md) |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Found: mesh_NACA0012_inv.su2
Found: solution_flow.dat
New Project: ./
Removing old designs in 10s. Done!

Sequential Least SQuares Programming (SLSQP) parameters:
Number of design variables: 38 ( 38 )
Objective function scaling factor: [1.0]
Maximum number of iterations: 100
Requested accuracy: 1e-16
Initial guess for the independent variable(s): [0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0]
Lower and upper bound for each independent variable: [(-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001), (-0.0001, 0.0001)]

Traceback (most recent call last):
File "D:\SU2-v8.0.0-win64\bin\shape_optimization.py", line 306, in <module>
main()
File "D:\SU2-v8.0.0-win64\bin\shape_optimization.py", line 184, in main
shape_optimization(
File "D:\SU2-v8.0.0-win64\bin\shape_optimization.py", line 282, in shape_optimization
SU2.opt.SLSQP(project, x0, xb, its, accu)
File "D:\SU2-v8.0.0-win64\bin\SU2\opt\scipy_tools.py", line 128, in scipy_slsqp
outputs = fmin_slsqp(
^^^^^^^^^^^
File "D:\python\Lib\site-packages\scipy\optimize\_slsqp_py.py", line 210, in fmin_slsqp
res = _minimize_slsqp(func, x0, args, jac=fprime, bounds=bounds,
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ ^^^^^^^^
File "D:\python\Lib\site-packages\scipy\optimize\_slsqp_py.py", line 383, in _minimize_slsqp
sf = _prepare_scalar_function(func, x, jac=jac, args=args, epsilon=eps,
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ ^^^^^^^^^^^^^^^^
File "D:\python\Lib\site-packages\scipy\optimize\_optimize.py", line 402, in _prepare_scalar_function
sf = ScalarFunction(fun, x0, args, grad, hess,
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "D:\python\Lib\site-packages\scipy\optimize\_differentiable_functions. py", line 166, in __init__
self._update_fun()
File "D:\python\Lib\site-packages\scipy\optimize\_differentiable_functions. py", line 262, in _update_fun
self._update_fun_impl()
File "D:\python\Lib\site-packages\scipy\optimize\_differentiable_functions. py", line 163, in update_fun
self.f = fun_wrapped(self.x)
^^^^^^^^^^^^^^^^^^^
File "D:\python\Lib\site-packages\scipy\optimize\_differentiable_functions. py", line 145, in fun_wrapped
fx = fun(np.copy(x), *args)
^^^^^^^^^^^^^^^^^^^^^^
File "D:\SU2-v8.0.0-win64\bin\SU2\opt\scipy_tools.py", line 416, in obj_f
obj_list = project.obj_f(x)
^^^^^^^^^^^^^^^^
File "D:\SU2-v8.0.0-win64\bin\SU2\opt\project.py", line 243, in obj_f
return self._eval(konfig, func, dvs)
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "D:\SU2-v8.0.0-win64\bin\SU2\opt\project.py", line 211, in _eval
vals = design._eval(func, *args)
^^^^^^^^^^^^^^^^^^^^^^^^^
File "D:\SU2-v8.0.0-win64\bin\SU2\eval\design.py", line 151, in _eval
vals = eval_func(*inputs)
^^^^^^^^^^^^^^^^^^
File "D:\SU2-v8.0.0-win64\bin\SU2\eval\design.py", line 250, in obj_f
func += su2func(this_obj, config, state) * sign * scale * global_factor
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "D:\SU2-v8.0.0-win64\bin\SU2\eval\functions.py", line 97, in function
aerodynamics(config, state)
File "D:\SU2-v8.0.0-win64\bin\SU2\eval\functions.py", line 285, in aerodynamics
info = su2run.direct(config)
^^^^^^^^^^^^^^^^^^^^^
File "D:\SU2-v8.0.0-win64\bin\SU2\run\direct.py", line 78, in direct
SU2_CFD(konfig)
File "D:\SU2-v8.0.0-win64\bin\SU2\run\interface.py", line 114, in CFD
run_command(the_Command)
File "D:\SU2-v8.0.0-win64\bin\SU2\run\interface.py", line 290, in run_command
raise exception(message)
SU2.EvaluationFailure: Path = D:\SU2\Naopt\DESIGNS\DSN_001\DIRECT\,
Command = "D:\bin\SU2_CFD" config_CFD.cfg
SU2 process returned error '1'
The system cannot find the path specified.

[bigfootedrockmidget]

So what is the error?

[kh3]

Originally Posted by bigfootedrockmidget

So what is the error?

When I run this two line in powershell
PS C:\Windows\System32\WindowsPowerShell\v1.0> cd D:\SU2\Naopt\
PS D:\SU2\Naopt> D:\SU2-v8.0.0-win64\bin\shape_optimization.py -g


And I got this, but the DIRECT file is create when I run these two lines.

CONTINUOUS_ADJOINT -o SLSQP -f inv_NACA0012_basic.cfg
SU2.EvaluationFailure: Path = D:\SU2\Naopt\DESIGNS\DSN_001\DIRECT\,
Command = "D:\bin\SU2_CFD" config_CFD.cfg
SU2 process returned error '1'
The system cannot find the path specified.