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| class | advectiveFvPatchField< Type > |
| | This boundary condition provides an advective outflow condition, based on solving DDt(W, field) = 0 at the boundary where W is the wave velocity and field is the field to which this boundary condition is applied. More...
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| class | fanPressureFvPatchScalarField |
| | This boundary condition can be applied to assign either a pressure inlet or outlet total pressure condition for a fan. More...
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| class | fixedNormalInletOutletVelocityFvPatchVectorField |
| | This velocity inlet/outlet boundary condition combines a fixed normal component obtained from the "normalVelocity" patchField supplied with a fixed or zero-gradiented tangential component depending on the direction of the flow and the setting of "fixTangentialInflow": More...
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| class | flowRateOutletVelocityFvPatchVectorField |
| | Velocity outlet boundary condition which corrects the extrapolated velocity to match the specified flow rate. More...
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| class | fluxCorrectedVelocityFvPatchVectorField |
| | This boundary condition provides a velocity outlet boundary condition for patches where the pressure is specified. The outflow velocity is obtained by "zeroGradient" and then corrected from the flux: More...
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| class | freestreamFvPatchField< Type > |
| | This boundary condition provides a free-stream condition. It is a 'mixed' condition derived from the inletOutlet condition, whereby the mode of operation switches between fixed (free stream) value and zero gradient based on the sign of the flux. More...
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| class | freestreamPressureFvPatchScalarField |
| | This boundary condition provides a free-stream condition for pressure. It is a zero-gradient condition that constrains the flux across the patch based on the free-stream velocity. More...
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| class | inletOutletFvPatchField< Type > |
| | This boundary condition provides a generic outflow condition, with specified inflow for the case of return flow. More...
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| class | inletOutletTotalTemperatureFvPatchScalarField |
| | This boundary condition provides an outflow condition for total temperature for use with supersonic cases, where a user-specified value is applied in the case of reverse flow. More...
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| class | matchedFlowRateOutletVelocityFvPatchVectorField |
| | Velocity outlet boundary condition which corrects the extrapolated velocity to match the flow rate of the specified corresponding inlet patch. More...
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| class | outletPhaseMeanVelocityFvPatchVectorField |
| | This boundary condition adjusts the velocity for the given phase to achieve the specified mean thus causing the phase-fraction to adjust according to the mass flow rate. More...
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| class | pressureDirectedInletOutletVelocityFvPatchVectorField |
| | This velocity inlet/outlet boundary condition is applied to pressure boundaries where the pressure is specified. A zero-gradient condtion is applied for outflow (as defined by the flux); for inflow, the velocity is obtained from the flux with the specified inlet direction. More...
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| class | pressureInletOutletParSlipVelocityFvPatchVectorField |
| | This velocity inlet/outlet boundary condition for pressure boundary where the pressure is specified. A zero-gradient is applied for outflow (as defined by the flux); for inflow, the velocity is obtained from the flux with the specified inlet direction. More...
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| class | pressureInletOutletVelocityFvPatchVectorField |
| | This velocity inlet/outlet boundary condition is applied to pressure boundaries where the pressure is specified. A zero-gradient condition is applied for outflow (as defined by the flux); for inflow, the velocity is obtained from the patch-face normal component of the internal-cell value. More...
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| class | pressureNormalInletOutletVelocityFvPatchVectorField |
| | This velocity inlet/outlet boundary condition is applied to patches where the pressure is specified. A zero-gradient condition is applied for outflow (as defined by the flux); for inflow, the velocity is obtained from the flux with a direction normal to the patch faces. More...
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| class | rotatingPressureInletOutletVelocityFvPatchVectorField |
| | This velocity inlet/outlet boundary condition is applied to patches in a rotating frame where the pressure is specified. A zero-gradient is applied for outflow (as defined by the flux); for inflow, the velocity is obtained from the flux with a direction normal to the patch faces. More...
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| class | rotatingTotalPressureFvPatchScalarField |
| | This boundary condition provides a total pressure condition for patches in a rotating frame. More...
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| class | supersonicFreestreamFvPatchVectorField |
| | This boundary condition provides a supersonic free-stream condition. More...
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| class | totalPressureFvPatchScalarField |
| | This boundary condition provides a total pressure condition. Four variants are possible: More...
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| class | totalTemperatureFvPatchScalarField |
| | This boundary condition provides a total temperature condition. More...
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| class | uniformInletOutletFvPatchField< Type > |
| | Variant of inletOutlet boundary condition with uniform inletValue. More...
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| class | uniformTotalPressureFvPatchScalarField |
| | This boundary condition provides a time-varying form of the uniform total pressure boundary condition Foam::totalPressureFvPatchField. More...
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| class | waveTransmissiveFvPatchField< Type > |
| | This boundary condition provides a wave transmissive outflow condition, based on solving DDt(W, field) = 0 at the boundary W is the wave velocity and field is the field to which this boundary condition is applied. More...
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1.8.13
