JPL Version 2.7
JetPropulsion Library 2.7 is part of Modelon���s 2024.1 release.
New versions of Modelon libraries are sold and distributed directly from Modelon, as well as approved resellers.
New features
- Added moist air variants of natural gas with combustion media packages with lumped dry air and an air mixture using NASA7 properties.
- Variable geometry nozzle capabilities for both throat and exit area. This is demonstrated in Experiments.MixedTurbofan.VariableNozzle
- More accurate efficiency correction models for compressors and turbines. Compute the efficiency with correlations taking reynolds number index, entry into service, size (corrected flow) and stage loading into account. They use of these are demonstrated in the new multi-point experiment model Turboprop.MultipointWithEfficiencyCorrection
Improvements
- Added support for the new Moist Air media with the JetPropulsion.Utilities.Adapters.Adapter. MoistAir and MoistAirMixture variants with Kerosene or NaturalGas can be adapted to a compatible media package for use with Modelon Base Library components. See the adapter documentation for more details.
- Mass estimate model JetPropulsion.Basic.MassEstimate.Nozzles.Onat1979 supports axisymmetric nozzle core.
- Mass estimate model JetPropulsion.Basic.MassEstimate.Burners.Onat1979 supports for automatic computation of geometry based on neighbouring components, as well as manual modification of flow velocity.
- Mass estimate model JetPropulsion.Basic.MassEstimate.Ducts.Onat1979Kaiser2020 support automatic computation of geometry based on neighbouring components, if Kaiser2020 option is selected.
Corrected nozzle exit station numbers
- core nozzle exit: 8 ��� 9
- core nozzle exit ideal: 8id ��� 9id
- bypass nozzle exit: 18 ��� 19
- bypass nozzle exit ideal: 18id ��� 19id
Fixed Issues
- Correcting temperature bounds for Walsh and Fletcher polynomials based on reference (200K - 2200K, which is broader than shown in the reference with 2000K). See the ���Conversion of user libraries��� section for more information
- Corrected the computation of the substance mass fractions downstream of the mixer.
- Corrected computation for compressor geometry change between outlet and inlet in JetPropulsion.Basic.MassEstimate.Compressors.Onat1979Axial
Library structure changes
New classes
- JetPropulsion.Media.PreDefined.MoistAirMixtureKerosene
- JetPropulsion.Utilities.Adapters.MediaMBL.MoistAirMixtureKerosene
- JetPropulsion.Media.PreDefined.MoistAirNaturalGas
- JetPropulsion.Media.PreDefined.MoistAirMixtureNaturalGas
- JetPropulsion.Utilities.Adapters.MediaMBL.MoistAirNaturalGas
- JetPropulsion.Utilities.Adapters.MediaMBL.MoistAirMixtureNaturalGas
- JetPropulsion.Basic.Nozzles.Experiments.VariableGeometry
- JetPropulsion.Basic.Nozzles.VariableGeometry
- JetPropulsion.Experiments.MixedTurbofan.VariableNozzle
- JetPropulsion.CyclePerformance.Control.Nozzle.ARFromAthqthDes_parabolic
- JetPropulsion.CyclePerformance.Control.Nozzle.AthqthDesFromPr
- JetPropulsion.CyclePerformance.Control.Nozzle.AthqthDesFromRline
- JetPropulsion.Experiments.Turboprop.MultipointWithEfficiencyCorrection
- JetPropulsion.CyclePerformance.Control.Boundary.FlowRateFromBurnerOutletTempPowerScheduled
- JetPropulsion.CyclePerformance.Control.Boundary.FlowRateFromTurbineTemp
- JetPropulsion.CyclePerformance.Control.Burner.FarFromTotalPower
- JetPropulsion.CyclePerformance.Control.Compressor.OverallPressureRatioPowerScheduled
- JetPropulsion.Basic.Turbines.EfficiencyCorrection
- JetPropulsion.Basic.Compressors.EfficiencyCorrection
- JetPropulsion.Basic.Turbines.Correlations.EfficiencyCorrection
- JetPropulsion.Basic.Compressors.Correlations.EfficiencyCorrection.Examples
- JetPropulsion.Basic.Compressors.Correlations.EfficiencyCorrection.Samuelsson2015
- JetPropulsion.Basic.Compressors.Correlations.EfficiencyCorrection.Samuelsson2015Polynomial
Moved classes
- JetPropulsion.Basic.MassEstimate.Ducts.Onat1979 ��� JetPropulsion.Basic.MassEstimate.Ducts.Onat1979Kaiser2020