Environment - simulationEnvironment:
startTime=0
stopTime=5
tolerance=1e-06
numberOfIntervals=2500
stepSize=0.002
Regular simulation: ./ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia  -abortSlowSimulation -alarm=480 -lv LOG_STATS
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_STDOUT        | warning | Non-Linear Solver try to handle a problem with a called assert.
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -135733 should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -1356.34 should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_STDOUT        | warning | While solving non-linear system an assertion failed during initialization.
|                 | |       | | The non-linear solver tries to solve the problem that could take some time.
|                 | |       | | It could help to provide better start-values for the iteration variables.
|                 | |       | | For more information simulate with -lv LOG_NLS_V
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -9999 should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -7.03411 should be >= 0
LOG_NLS           | error   | residualFunc662: Iteration variable `CombustionChamber1.fluegas.R_s` is inf or nan.
LOG_ASSERT        | debug   | residualFunc662 failed at time=0.
|                 | |       | For more information please use -lv LOG_NLS.
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -7.03411 should be >= 0
LOG_NLS           | error   | residualFunc662: Iteration variable `CombustionChamber1.fluegas.R_s` is inf or nan.
LOG_ASSERT        | debug   | residualFunc662 failed at time=0.
|                 | |       | For more information please use -lv LOG_NLS.
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.0203041 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.00590776 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.00590776 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.297394)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -2.60491 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.0203041 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.297394)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -2.60491 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.297394)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -2.60491 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -7.03411 should be >= 0
LOG_NLS           | error   | residualFunc662: Iteration variable `CombustionChamber1.fluegas.R_s` is inf or nan.
LOG_ASSERT        | debug   | residualFunc662 failed at time=0.
|                 | |       | For more information please use -lv LOG_NLS.
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.0203041 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -7.03411 should be >= 0
LOG_NLS           | error   | residualFunc662: Iteration variable `CombustionChamber1.fluegas.R_s` is inf or nan.
LOG_ASSERT        | debug   | residualFunc662 failed at time=0.
|                 | |       | For more information please use -lv LOG_NLS.
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.0203041 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -7.03411 should be >= 0
LOG_NLS           | error   | residualFunc662: Iteration variable `CombustionChamber1.fluegas.R_s` is inf or nan.
LOG_ASSERT        | debug   | residualFunc662 failed at time=0.
|                 | |       | For more information please use -lv LOG_NLS.
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.0203041 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -7.03411 should be >= 0
LOG_NLS           | error   | residualFunc662: Iteration variable `CombustionChamber1.fluegas.R_s` is inf or nan.
LOG_ASSERT        | debug   | residualFunc662 failed at time=0.
|                 | |       | For more information please use -lv LOG_NLS.
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.0203041 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -7.03411 should be >= 0
LOG_NLS           | error   | residualFunc662: Iteration variable `CombustionChamber1.fluegas.R_s` is inf or nan.
LOG_ASSERT        | debug   | residualFunc662 failed at time=0.
|                 | |       | For more information please use -lv LOG_NLS.
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.0203041 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-0.220283)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -0.219441 should be >= 0
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | debug   | ThermoPower_4.0.0-dev_ThermoPower.Test.GasComponents.TestTurboJetInertia_functions.c:4155: Invalid root: (-36.5304)^(0.277189)
LOG_ASSERT        | warning | The following assertion has been violated during initialization at time 0.000000
LOG_ASSERT        | debug   | Model error: Argument of sqrt(1.0 - (1.0 / Turbine1.PR) ^ 2.0) was -inf should be >= 0
LOG_ASSERT        | debug   | Solving non-linear system 662 failed at time=0.
|                 | |       | For more information please use -lv LOG_NLS.
LOG_ASSERT        | error   | Failed to solve the initialization problem with global homotopy with equidistant step size.
LOG_ASSERT        | debug   | Unable to solve initialization problem.
LOG_ASSERT        | info    | simulation terminated by an assertion at initialization