modelFlow1D

1-dimensional fluid flow model for gas (finite volumes)
Diagram of Flow1D

Extends from Modelica.Icons.ObsoleteModel (Icon for classes that are obsolete and will be removed in later versions), Icons.Gas.Tube.

Information

This model describes the flow of a gas in a rigid tube. The basic modelling assumptions are:

  • Uniform velocity is assumed on the cross section, leading to a 1-D distributed parameter model.
  • Turbulent friction is always assumed; a small linear term is added to avoid numerical singularities at zero flowrate. The friction effects are not accurately computed in the laminar and transitional flow regimes, which however should not be an issue in most power generation applications.
  • The model is based on dynamic mass, momentum, and energy balances. The dynamic momentum term can be switched off, to avoid the fast oscillations that can arise from its coupling with the mass balance (sound wave dynamics).
  • The longitudinal heat diffusion term is neglected.
  • The energy balance equation is written by assuming a uniform pressure distribution; the pressure drop is lumped either at the inlet or at the outlet.
  • The fluid flow can exchange thermal power through the lateral surface, which is represented by the wall connector. The actual heat flux must be computed by a connected component (heat transfer computation module).

The mass, momentum and energy balance equation are discretised with the finite volume method. The state variables are one pressure, one flowrate (optional), N-1 temperatures, and either one or N-1 gas composition vectors.

The turbulent friction factor can be either assumed as a constant, or computed by Colebrook's equation. In the former case, the friction factor can be supplied directly, or given implicitly by a specified operating point. In any case, the multiplicative correction coefficient Kfc can be used to modify the friction coefficient, e.g. to fit experimental data.

A small linear pressure drop is added to avoid numerical singularities at low or zero flowrate. The wnom parameter must be always specified: the additional linear pressure drop is such that it is equal to the turbulent pressure drop when the flowrate is equal to wnf*wnom (the default value is 1% of the nominal flowrate). Increase wnf if numerical problems occur in tubes with very low pressure drops.

Flow reversal is fully supported.

Modelling options

The actual gas used in the component is determined by the replaceable Medium package.In the case of multiple component, variable composition gases, the start composition is given by Xstart, whose default value is Medium.reference_X.

Thermal variables (enthalpy, temperature, density) are computed in N equally spaced nodes, including the inlet (node 1) and the outlet (node N); N must be greater than or equal to 2.

if UniformComposition is true, then a uniform compostion is assumed for the gas through the entire tube length; otherwise, the gas compostion is computed in N equally spaced nodes, as in the case of thermal variables.

The following options are available to specify the friction coefficient:

  • FFtype = FFtypes.Kfnom: the hydraulic friction coefficient Kf is set directly to Kfnom.
  • FFtype = FFtypes.OpPoint: the hydraulic friction coefficient is specified by a nominal operating point (wnom,dpnom, rhonom).
  • FFtype = FFtypes.Cfnom: the friction coefficient is computed by giving the (constant) value of the Fanning friction factor Cfnom.
  • FFtype = FFtypes.Colebrook: the Fanning friction factor is computed by Colebrook's equation (assuming Re > 2100, e.g. turbulent flow).
  • FFtype = FFtypes.NoFriction: no friction is assumed across the pipe.

If QuasiStatic is set to true, the dynamic terms are neglected in the mass, momentum, and energy balances, i.e., quasi-static behaviour is modelled. It is also possible to neglect only the dynamic momentum term by setting DynamicMomentum = false.

If HydraulicCapacitance = 2 (default option) then the mass buildup term depending on the pressure is lumped at the outlet, while the optional momentum buildup term depending on the flowrate is lumped at the inlet; therefore, the state variables are the outlet pressure and the inlet flowrate. If HydraulicCapacitance = 1 the reverse takes place.

Start values for the pressure and flowrate state variables are specified by pstart, wstart. The start values for the node temperatures are linearly distributed from Tstartin at the inlet to Tstartout at the outlet. The (uniform) start value of the gas composition is specified by Xstart.

A bank of Nt identical tubes working in parallel can be modelled by setting Nt > 1. The geometric parameters always refer to a single tube.

This models makes the temperature and external heat flow distributions available to connected components through the wall connector. If other variables (e.g. the heat transfer coefficient) are needed by external components to compute the actual heat flow, the wall connector can be replaced by an extended version of the DHT connector.

Parameters

TypeNameDefaultDescription
IntegerN2Number of nodes for thermal variables
IntegerNt1Number of tubes in parallel
SI.DistanceLTube length
SI.PositionH0Elevation of outlet over inlet
SI.AreaACross-sectional area (single tube)
SI.LengthomegaPerimeter of heat transfer surface (single tube)
SI.LengthDhydHydraulic Diameter (single tube)
Medium.MassFlowRatewnomNominal mass flowrate (total)
FFtypesFFtypeFriction Factor Type
RealKfnom0Nominal hydraulic resistance coefficient
SI.PressureDifferencedpnom0Nominal pressure drop
Medium.Densityrhonom0Nominal inlet density
SI.PerUnitCfnom0Nominal Fanning friction factor
SI.PerUnite0Relative roughness (ratio roughness/diameter)
BooleanDynamicMomentumfalseInertial phenomena accounted for
BooleanUniformCompositiontrueUniform gas composition is assumed
BooleanQuasiStaticfalseQuasi-static model (mass, energy and momentum static balances
HCtypesHydraulicCapacitanceHCtypes.Downstream1: Upstream, 2: Downstream
BooleanavoidInletEnthalpyDerivativetrueAvoid inlet enthalpy derivative
BooleanallowFlowReversalsystem.allowFlowReversal= true to allow flow reversal, false restricts to design direction
SI.Velocityunom10Nominal velocity for simplified equation
SI.PerUnitwnf0.01Fraction of nominal flow rate at which linear friction equals turbulent friction
SI.PerUnitKfc1Friction factor correction coefficient
Initialisation
Medium.AbsolutePressurepstart1e5Pressure start value
Medium.TemperatureTstartbar300Avarage temperature start value
Medium.TemperatureTstartinTstartbarInlet temperature start value
Medium.TemperatureTstartoutTstartbarOutlet temperature start value
Medium.Temperature[N]Tstartlinspace(Tstartin, Tstartout, N)Start value of temperature vector (initialized by default)
Medium.MassFraction[nX]XstartMedium.reference_XStart gas composition
Choices.Init.OptionsinitOptChoices.Init.Options.noInitInitialisation option

Connectors

TypeNameDefaultDescription
FlangeAinfl
FlangeBoutfl
Thermal.DHTwall

Components

TypeNameDefaultDescription
ThermoPower.SystemsystemSystem wide properties
Medium.BaseProperties[N]gasGas nodal properties
SI.PressureDpfricPressure drop due to friction
SI.Lengthomega_hydWet perimeter (single tube)
RealKfFriction factor
RealKflLinear friction factor
RealdwdtTime derivative of mass flow rate
SI.PerUnitCfFanning friction factor
Medium.MassFlowRatewMass flowrate (single tube)
Medium.Temperature[N - 1]TtildeTemperature state variables
Medium.TemperatureTin
Medium.MassFraction[if UniformComposition or Medium.fixedX then 1 else N - 1,nX]XtildeComposition state variables
Medium.MassFlowRate[N - 1]wbar
SI.Velocity[N]uFluid velocity
Medium.AbsolutePressurep
SI.TimeTrResidence time
SI.MassMGas Mass
SI.PowerQTotal heat flow through the wall (all Nt tubes)

Contents

NameDescription
Medium
squareReg

Revisions