(su) root01@root01-virtual-machine:~/plate24degree/uniform$ valgrind SU2_CFD config_sst.cfg ==12657== Memcheck, a memory error detector ==12657== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al. ==12657== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info ==12657== Command: SU2_CFD config_sst.cfg ==12657== ------------------------------------------------------------------------- | ___ _ _ ___ | | / __| | | |_ ) Release 8.0.1 "Harrier" | | \__ \ |_| |/ / | | |___/\___//___| Suite (Computational Fluid Dynamics Code) | | | ------------------------------------------------------------------------- | SU2 Project Website: https://su2code.github.io | | | | The SU2 Project is maintained by the SU2 Foundation | | (http://su2foundation.org) | ------------------------------------------------------------------------- | Copyright 2012-2024, SU2 Contributors | | | | 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 . | ------------------------------------------------------------------------- Parsing config file for zone 0 ----------------- Physical Case Definition ( Zone 0 ) ------------------- Compressible RANS equations. Turbulence model: Menter's k-omega SST-2003m with no production modification. Hybrid RANS/LES: No Hybrid RANS/LES Mach number: 2.84. Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg. Reynolds number: 0. Reference length 3. No restart solution, use the values at infinity (freestream). Non-Dimensional simulation (V=Mach, Rho=1.0, T=1.0 at the farfield). The reference area is 3 m^2. The semi-span will be computed using the max y(3D) value. The reference length is 3 m. Reference origin for moment evaluation is (0, 0, 0). Surface(s) where the force coefficients are evaluated: lower. Surface(s) plotted in the output file: lower. Input mesh file name: mesh.su2 --------------- Space Numerical Integration ( Zone 0 ) ------------------ HLLC solver for the flow inviscid terms. Standard Roe without low-dissipation function. Second order integration in space, with slope limiter. Venkatakrishnan slope-limiting method, with constant: 0.05. The reference element size is: 1. Scalar upwind solver for the turbulence model. First order integration in space. Average of gradients with correction (viscous flow terms). Average of gradients with correction (viscous turbulence terms). Gradient for upwind reconstruction: Green-Gauss. Gradient for viscous and source terms: Green-Gauss. --------------- Time Numerical Integration ( Zone 0 ) ------------------ Local time stepping (steady state simulation). Euler implicit method for the flow equations. FGMRES is used for solving the linear system. Using a ILU(0) preconditioning. Convergence criteria of the linear solver: 0.0001. Max number of linear iterations: 3. CFL adaptation. Factor down: 1, factor up: 1.05, lower limit: 1, upper limit: 100, acceptable linear residual: 0.8. Courant-Friedrichs-Lewy number: 1 Euler implicit time integration for the turbulence model. ------------------ Convergence Criteria ( Zone 0 ) --------------------- Maximum number of solver subiterations: 10000. Begin convergence monitoring at iteration 5. Residual minimum value: 1e-10. Cauchy series min. value: 1e-10. Number of Cauchy elements: 100. Begin windowed time average at iteration 0. -------------------- Output Information ( Zone 0 ) ---------------------- File writing frequency: +------------------------------------+ | File| Frequency| +------------------------------------+ | RESTART| 200| | PARAVIEW| 200| | SURFACE_PARAVIEW| 200| +------------------------------------+ Writing the convergence history file every 1 inner iterations. Writing the screen convergence history every 1 inner iterations. The tabular file format is CSV (.csv). Convergence history file name: history. Forces breakdown file name: forces_breakdown.dat. Surface file name: surface. Volume file name: vol_solution. Restart file name: restart.dat. ------------- Config File Boundary Information ( Zone 0 ) --------------- +-----------------------------------------------------------------------+ | Marker Type| Marker Name| +-----------------------------------------------------------------------+ | Symmetry plane| symmetry| +-----------------------------------------------------------------------+ | Supersonic inlet boundary| inlet| +-----------------------------------------------------------------------+ | Outlet boundary| outlet| +-----------------------------------------------------------------------+ | Heat flux wall| lower| +-----------------------------------------------------------------------+ -------------------- Output Preprocessing ( Zone 0 ) -------------------- WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...) Screen output fields: INNER_ITER, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, RMS_TKE, RMS_DISSIPATION, FORCE_X, LINSOL_RESIDUAL, AVG_CFL History output group(s): ITER, RMS_RES, AERO_COEFF Convergence field(s): RMS_DENSITY Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive. Volume output fields: COORDINATES, SOLUTION, PRIMITIVE ------------------- Geometry Preprocessing ( Zone 0 ) ------------------- Two dimensional problem. 114152 grid points. 113250 volume elements. 4 surface markers. 151 boundary elements in index 0 (Marker = inlet). 750 boundary elements in index 1 (Marker = symmetry). 151 boundary elements in index 2 (Marker = outlet). 750 boundary elements in index 3 (Marker = lower). 113250 quadrilaterals. Setting point connectivity. Renumbering points (Reverse Cuthill McKee Ordering). Recomputing point connectivity. Setting element connectivity. Checking the numerical grid orientation. There has been a re-orientation of 113250 QUADRILATERAL volume elements. There has been a re-orientation of 1802 LINE surface elements. Identifying edges and vertices. Setting the control volume structure. Area of the computational grid: 0.6096. Searching for the closest normal neighbors to the surfaces. Storing a mapping from global to local point index. Compute the surface curvature. Max K: 499.993. Mean K: 1.61092. Standard deviation K: 25.7982. Checking for periodicity. Computing mesh quality statistics for the dual control volumes. +--------------------------------------------------------------+ | Mesh Quality Metric| Minimum| Maximum| +--------------------------------------------------------------+ | Orthogonality Angle (deg.)| 90| 90| | CV Face Area Aspect Ratio| 1.01279| 366.417| | CV Sub-Volume Ratio| 1| 1.04| +--------------------------------------------------------------+ Finding max control volume width. Wetted area = 3 m. Area projection in the x-plane = 0 m, y-plane = 0 m. Max. coordinate in the x-direction = 3 m, y-direction = 0 m. Min. coordinate in the x-direction = 0 m, y-direction = 0 m. Checking if Euler & Symmetry markers are straight/plane: Boundary marker symmetry is a single straight. Computing wall distances. -------------------- Solver Preprocessing ( Zone 0 ) -------------------- Viscous flow: Computing pressure using the ideal gas law based on the free-stream temperature and a density computed from the Reynolds number. Force coefficients computed using free-stream values. -- Models: +------------------------------------------------------------------------------+ | Viscosity Model| Conductivity Model| Fluid Model| +------------------------------------------------------------------------------+ | SUTHERLAND| CONSTANT_PRANDTL| STANDARD_AIR| +------------------------------------------------------------------------------+ -- Fluid properties: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Ref. Viscosity| 1.716e-05| 164.599| N.s/m^2| 1.04253e-07| | Sutherland Temp.| 273.15| 100.26| K| 2.72442| | Sutherland Const.| 110.4| 100.26| K| 1.10114| +------------------------------------------------------------------------------+ | Prandtl (Lam.)| -| -| -| 0.72| | Prandtl (Turb.)| -| -| -| 0.9| +------------------------------------------------------------------------------+ | Gas Constant| 287.058| 401.881| N.m/kg.K| 0.714286| | Spec. Heat Ratio| -| -| -| 1.4| +------------------------------------------------------------------------------+ -- Initial and free-stream conditions: +------------------------------------------------------------------------------+ | Name| Dim. value| Ref. value| Unit|Non-dim. value| +------------------------------------------------------------------------------+ | Static Pressure| 23600| 33040| Pa| 0.714286| | Density| 0.820002| 0.820002| kg/m^3| 1| | Temperature| 100.26| 100.26| K| 1| | Total Energy| 235662| 40292.6| m^2/s^2| 5.84876| | Velocity-X| 570.074| 200.73| m/s| 2.84| | Velocity-Y| 0| 200.73| m/s| 0| | Velocity Magnitude| 570.074| 200.73| m/s| 2.84| +------------------------------------------------------------------------------+ | Viscosity| 6.94779e-06| 164.599| N.s/m^2| 4.22104e-08| | Conductivity| -| 66149.3| W/m^2.K| -| | Turb. Kin. Energy| 1218.69| 40292.6| m^2/s^2| 0.030246| | Spec. Dissipation| 1.43834e+11| 200.73| 1/s| 7.16553e+08| +------------------------------------------------------------------------------+ | Mach Number| -| -| -| 2.84| | Reynolds Number| -| -| -| 2.01846e+08| +------------------------------------------------------------------------------+ Initialize Jacobian structure (Navier-Stokes). MG level: 0. Initialize Jacobian structure (SST model). Reading inlet profile from file: inletUNI.dat ==12657== Invalid read of size 8 ==12657== at 0xDD36EB: CConfig::GetInletPtotal(std::__cxx11::basic_string, std::allocator > const&) const (in /usr/local/bin/SU2_CFD) ==12657== by 0x659A5D: CSolver::LoadInletProfile(CGeometry**, CSolver***, CConfig*, int, unsigned short, unsigned short) const (in /usr/local/bin/SU2_CFD) ==12657== by 0x2BFEB3: CDriver::PreprocessInlet(CSolver***, CGeometry**, CConfig*) const (in /usr/local/bin/SU2_CFD) ==12657== by 0x2D6618: CDriver::CDriver(char*, unsigned short, int, bool) (in /usr/local/bin/SU2_CFD) ==12657== by 0x30B182: CSinglezoneDriver::CSinglezoneDriver(char*, unsigned short, int) (in /usr/local/bin/SU2_CFD) ==12657== by 0x25B64A: main (in /usr/local/bin/SU2_CFD) ==12657== Address 0x0 is not stack'd, malloc'd or (recently) free'd ==12657== ==12657== ==12657== Process terminating with default action of signal 11 (SIGSEGV) ==12657== Access not within mapped region at address 0x0 ==12657== at 0xDD36EB: CConfig::GetInletPtotal(std::__cxx11::basic_string, std::allocator > const&) const (in /usr/local/bin/SU2_CFD) ==12657== by 0x659A5D: CSolver::LoadInletProfile(CGeometry**, CSolver***, CConfig*, int, unsigned short, unsigned short) const (in /usr/local/bin/SU2_CFD) ==12657== by 0x2BFEB3: CDriver::PreprocessInlet(CSolver***, CGeometry**, CConfig*) const (in /usr/local/bin/SU2_CFD) ==12657== by 0x2D6618: CDriver::CDriver(char*, unsigned short, int, bool) (in /usr/local/bin/SU2_CFD) ==12657== by 0x30B182: CSinglezoneDriver::CSinglezoneDriver(char*, unsigned short, int) (in /usr/local/bin/SU2_CFD) ==12657== by 0x25B64A: main (in /usr/local/bin/SU2_CFD) ==12657== If you believe this happened as a result of a stack ==12657== overflow in your program's main thread (unlikely but ==12657== possible), you can try to increase the size of the ==12657== main thread stack using the --main-stacksize= flag. ==12657== The main thread stack size used in this run was 8388608. ==12657== ==12657== HEAP SUMMARY: ==12657== in use at exit: 386,942,531 bytes in 480,219 blocks ==12657== total heap usage: 5,850,550 allocs, 5,370,331 frees, 712,664,049 bytes allocated ==12657== ==12657== LEAK SUMMARY: ==12657== definitely lost: 0 bytes in 0 blocks ==12657== indirectly lost: 0 bytes in 0 blocks ==12657== possibly lost: 17,843 bytes in 330 blocks ==12657== still reachable: 386,924,688 bytes in 479,889 blocks ==12657== of which reachable via heuristic: ==12657== newarray : 3,000 bytes in 31 blocks ==12657== suppressed: 0 bytes in 0 blocks ==12657== Rerun with --leak-check=full to see details of leaked memory ==12657== ==12657== For lists of detected and suppressed errors, rerun with: -s ==12657== ERROR SUMMARY: 1 errors from 1 contexts (suppressed: 0 from 0) 段错误 (核心已转储) (su) root01@root01-virtual-machine:~/plate24degree/uniform$