/home/hudson/saved_omc/OMSimulator/install/bin/OMSimulator -r=ClaRa_ClaRa.Components.TurboMachines.Turbines.Check.testStackedTurbineStages_res.mat --tempDir=temp_ClaRa_ClaRa_Components_TurboMachines_Turbines_Check_testStackedTurbineStages_fmu --startTime=0 --stopTime=20 --stepSize=0.008 --timeout=800 --tolerance=1e-06 ClaRa_ClaRa_Components_TurboMachines_Turbines_Check_testStackedTurbineStages.fmu warning: Failed to load settings: [json.exception.parse_error.101] parse error at line 4, column 1: syntax error while parsing value - unexpected '}'; expected end of input warning: Failed to save settings: [json.exception.parse_error.101] parse error at line 4, column 1: syntax error while parsing value - unexpected '}'; expected end of input info: Set temp directory to "/var/lib/jenkins1/ws/OpenModelicaLibraryTestingWork/OpenModelicaLibraryTesting/ClaRa_ClaRa.Components.TurboMachines.Turbines.Check.testStackedTurbineStages" info: Set working directory to "/var/lib/jenkins1/ws/OpenModelicaLibraryTestingWork/OpenModelicaLibraryTesting/ClaRa_ClaRa.Components.TurboMachines.Turbines.Check.testStackedTurbineStages" info: New model "model" with corresponding temp directory "/var/lib/jenkins1/ws/OpenModelicaLibraryTestingWork/OpenModelicaLibraryTesting/ClaRa_ClaRa.Components.TurboMachines.Turbines.Check.testStackedTurbineStages/model-mxjlnmx8" info: Set working directory to "/var/lib/jenkins1/ws/OpenModelicaLibraryTestingWork/OpenModelicaLibraryTesting/ClaRa_ClaRa.Components.TurboMachines.Turbines.Check.testStackedTurbineStages" info: *** FMU Simulation Info *** - model: model (co-simulation) - path: ClaRa_ClaRa_Components_TurboMachines_Turbines_Check_testStackedTurbineStages.fmu - startTime: 0.000000 - stopTime: 20.000000 - tolerance: 0.000001 - stepSize: 0.008000 LOG_SOLVER | info | CVODE linear multistep method CV_BDF LOG_SOLVER | info | CVODE maximum integration order CV_ITER_NEWTON LOG_SOLVER | info | CVODE use equidistant time grid YES LOG_SOLVER | info | CVODE Using relative error tolerance 1.000000e-06 LOG_SOLVER | info | CVODE Using dense internal linear solver SUNLinSol_Dense. LOG_SOLVER | info | CVODE Use internal dense numeric jacobian method. LOG_SOLVER | info | CVODE uses internal root finding method NO LOG_SOLVER | info | CVODE maximum absolut step size 0 LOG_SOLVER | info | CVODE initial step size is set automatically LOG_SOLVER | info | CVODE maximum integration order 5 LOG_SOLVER | info | CVODE maximum number of nonlinear convergence failures permitted during one step 10 LOG_SOLVER | info | CVODE BDF stability limit detection algorithm OFF LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[5], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=17): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[5], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=17): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[5], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=17): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[4], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=15): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[4], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=15): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[4], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=15): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[3], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=13): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[3], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=13): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[3], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=13): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[2], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=11): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[2], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=11): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[2], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=11): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[1], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=9): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[1], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=9): negative pressure (p=0.000000)! Stopping property calculation! LOG_STDOUT | info | TILMedia-Error(testStackedTurbineStages.GasFanAdvanced.OutletNom[1], GM_GasMixtureModel_setSimpleCondensingProperties_pTxi, mediumPointerID=9): negative pressure (p=0.000000)! Stopping property calculation! LOG_ASSERT | debug | division by zero at time 0, (a=1) / (b=0), where divisor b expression is: GasFanAdvanced.p_out_nom_st[1] error: [fmi2logger] [fmi2Error] ClaRa_ClaRa_Components_TurboMachines_Turbines_Check_testStackedTurbineStages/logFmi2Call: fmi2ExitInitializationMode: terminated by an assertion. error: [initialize] fmi2_exitInitializationMode failed for FMU "model.root.ClaRa_ClaRa_Components_TurboMachines_Turbines_Check_testStackedTurbineStages" error: [initialize] Initialization of system "model.root" failed error: [SimulateSingleFMU] oms_initialize failed info: 2 warnings info: 4 errors