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a question about parallel in windows 7
I want to Parallel compute a file in windows 64,the computer is installed :
mpich2-1.4.1p1-win-ia32.msi SU2-3.0.000-64-bit-Parallel.exe python 2.7 numpy and scipy When computing a file,I enter the "python parallel_computation.py -f turb_ONERAM6.cfg -p 2 " in cmd.exe and face the error: the command:mpiexec -np 2 D:\Program Files\SU2\SU2_DDC config_DDC.cfg the location: D:\ launch failed:CreateProcess<D:\Program Files\SU2\SU2_DDC config_DDC.cfg>on 'owner-PC' failed,error 2 -system can't the file launch failed:CreateProcess<D:\Program Files\SU2\SU2_DDC config_DDC.cfg>on 'owner-PC' failed,error 2 -system can't the file (.su2 and .cfg are located at D disk,the softare are located at D:\Program Files\SU2 and make environment variable as 'path' ) I want to the reason.Thanks |
Two issues:
- MPICH2 has discontinued Windows support entirely and hence SU^2 no longer supports it on the Windows platform. The executables are built with Microsoft's MPI implementation which can be downloaded for free as part of the "HPC pack". Please refer to the SU^2 Windows installation documentation for a link and details. - (Just an FYI) It looks like you're trying to run the 32-bit version of MPICH2 on a 64-bit Windows system. |
Quote:
D:\>parallel_computation.py -f inv_NACA0012.cfg -p 2 the command: mpiexec -np 2 C:\SU2\SU2_DDC config_DDC.cfg the location: D:\ WARNING: unrecognized option in the config. file: GRID_DEFORM_METHOD. WARNING: unrecognized option in the config. file: GRID_DEFORM_METHOD. ------------------------------------------------------------------------- | _____ _ _ ___ | | / ____| | | | | |__ \ Web: su2.stanford.edu | ------------------------------------------------------------------------- | _____ _ _ ___ | | / ____| | | | | |__ \ Web: su2.stanford.edu | | | (___ | | | | ) | Twitter: @su2code | | | (___ | | | | ) | Twitter: @su2code | | \___ \ | | | | / / Forum: www.cfd-online.com/Forums/su2/ | | ____) | | |__| | / /_ | | \___ \ | | | | / / Forum: www.cfd-online.com/Forums/su2/ | | ____) | | |__| | / /_ | | |_____/ \____/ |____| Suite (Domain Decomposition Code) | | |_____/ \____/ |____| Suite (Domain Decomposition Code) | | Release 2.0.10 | ------------------------------------------------------------------------- | Release 2.0.10 | | Stanford University Unstructured (SU2). | | Copyright (C) 2012-2013 Aerospace Design Laboratory (ADL). | | 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 (version 2.1) for more details. | ------------------------------------------------------------------------- ------------------------------------------------------------------------- ------------------------ Physical case definition ----------------------- Input mesh file name: mesh_NACA0012_inv.su2 | Stanford University Unstructured (SU2). | -------------------------- Output information --------------------------- | Copyright (C) 2012-2013 Aerospace Design Laboratory (ADL). | Don't visualize the partitions. ------------------- Config file boundary information -------------------- | 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 (version 2.1) for more details. | Euler wall boundary marker(s): airfoil. Far-field boundary marker(s): farfield. ------------------------------------------------------------------------- ------------------------ Physical case definition ----------------------- Input mesh file name: mesh_NACA0012_inv.su2 -------------------------- Output information --------------------------- Don't visualize the partitions. ------------------- Config file boundary information -------------------- Euler wall boundary marker(s): airfoil. Far-field boundary marker(s): farfield. ---------------------- Read grid file information ----------------------- Two dimensional problem. 10216 interior elements. 10216 triangles. 5233 points. 2 surface markers. 200 boundary elements in index 0 (Marker = airfoil). 50 boundary elements in index 1 (Marker = farfield). ------------------------ Divide the numerical grid ---------------------- ----------------------------- Write mesh files -------------------------- job aborted: [ranks] message [0] terminated [1] process exited without calling finalize ---- error analysis ----- [1] on XingYu-PC C:\SU2\SU2_DDC ended prematurely and may have crashed. exit code 0xc0000005 ---- error analysis ----- SU2 process was terminated by signal '3' I look forward to your answer,thank you so much! |
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