pyNastran
0.5.0
pyNastran BDF Reader/Writer, OP2 Parser, and GUI
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Public Member Functions | |
def | __init__ |
def | rawFields |
Public Attributes | |
sid | |
Trim set identification number. | |
mach | |
Mach number. | |
q | |
Dynamic pressure. | |
labels | |
The label identifying aerodynamic trim variables defined on an AESTAT or AESURF entry. | |
uxs | |
The magnitude of the aerodynamic extra point degree-of-freedom. | |
aeqr | |
Flag to request a rigid trim analysis (Real > 0.0 and < 1.0; Default =1.0. | |
Static Public Attributes | |
string | type = 'TRIM' |
def pyNastran.bdf.cards.aero.TRIM.__init__ | ( | self, | |
card = None , |
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data = None |
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) |
def pyNastran.bdf.cards.aero.TRIM.rawFields | ( | self | ) |
Definition at line 1301 of file aero.py.
Referenced by pyNastran.bdf.cards.baseCard.Property.__init__(), pyNastran.bdf.cards.elements.shell.CTRIAX.__init__(), pyNastran.bdf.cards.elements.shell.CSHEAR.Area(), pyNastran.bdf.cards.baseCard.BaseCard.buildTableLines(), pyNastran.bdf.cards.materials.MATS1.crossReference(), pyNastran.bdf.cards.loads.staticLoads.FORCE1.G2(), pyNastran.bdf.cards.baseCard.BaseCard.isSameCard(), pyNastran.bdf.cards.elements.springs.SpringElement.Mass(), pyNastran.bdf.cards.sets.ABCQSet.rawFields(), pyNastran.bdf.cards.nodes.SPOINTs.rawFields(), pyNastran.bdf.cards.dynamic.TSTEP.rawFields(), pyNastran.bdf.cards.thermal.loads.QHBDY.rawFields(), pyNastran.bdf.cards.loads.loads.SLOAD.rawFields(), pyNastran.bdf.cards.thermal.loads.TEMP.rawFields(), pyNastran.bdf.cards.loads.staticLoads.LOAD.rawFields(), pyNastran.bdf.cards.loads.loads.DLOAD.rawFields(), pyNastran.bdf.cards.methods.EIGP.rawFields(), pyNastran.bdf.cards.elements.mass.CONM1.rawFields(), pyNastran.bdf.cards.tables.TIC.rawFields(), pyNastran.bdf.cards.optimization.DVPREL2.rawFields(), pyNastran.bdf.cards.loads.staticLoads.PLOAD4.rawFields(), pyNastran.bdf.cards.properties.bars.PBEAML.rawFields(), pyNastran.bdf.cards.elements.elements.CFAST.reprFields(), pyNastran.bdf.cards.elements.damper.CVISC.reprFields(), pyNastran.bdf.cards.properties.mass.NSM.reprFields(), pyNastran.bdf.cards.properties.damper.PDAMP.reprFields(), pyNastran.bdf.cards.properties.mass.PMASS.reprFields(), pyNastran.bdf.cards.properties.damper.PDAMP5.reprFields(), pyNastran.bdf.cards.elements.springs.SpringElement.reprFields(), pyNastran.bdf.cards.tables.TABLED1.reprFields(), pyNastran.bdf.cards.properties.bush.PBUSH.reprFields(), pyNastran.bdf.cards.properties.damper.PDAMPT.reprFields(), pyNastran.bdf.cards.tables.TABLED2.reprFields(), pyNastran.bdf.cards.tables.TABLED3.reprFields(), pyNastran.bdf.cards.tables.TABLEM2.reprFields(), pyNastran.bdf.cards.tables.TABLEM3.reprFields(), pyNastran.bdf.cards.tables.TABLEM4.reprFields(), pyNastran.bdf.cards.properties.bush.PBUSH1D.reprFields(), pyNastran.bdf.cards.tables.TABLES1.reprFields(), pyNastran.bdf.cards.tables.TABLEST.reprFields(), pyNastran.bdf.cards.tables.TABRNDG.reprFields(), pyNastran.bdf.cards.elements.bars.CBEAM.reprFields(), pyNastran.bdf.cards.sets.Set.SetIDs(), pyNastran.bdf.cards.elements.bars.CROD.Stiffness1D(), pyNastran.bdf.cards.coordinateSystems.Coord.T(), and pyNastran.bdf.cards.loads.loads.RANDPS.Tid().
string pyNastran::bdf::cards::aero.TRIM::type = 'TRIM' [static] |
Reimplemented from pyNastran.bdf.cards.baseCard.BaseCard.
Definition at line 1263 of file aero.py.
Referenced by pyNastran.bdf.cards.nodes.Node::__init__(), pyNastran.bdf.cards.sets.ABQSet1::__init__(), pyNastran.bdf.cards.baseCard.Property::__init__(), pyNastran.bdf.cards.baseCard.Element::__init__(), pyNastran.bdf.cards.sets.CSET1::__init__(), pyNastran.bdf.cards.dmig.NastranMatrix::__repr__(), pyNastran.bdf.cards.elements.shell.ShellElement::Area(), pyNastran.bdf.cards.properties.bars.LineProperty::areaL(), pyNastran.bdf.cards.materials.MAT2::Dplate(), pyNastran.bdf.cards.loads.staticLoads.Force::F(), pyNastran.bdf.cards.elements.shell.ShellElement::flipNormal(), pyNastran.bdf.cards.dmig.NastranMatrix::getDType(), pyNastran.bdf.cards.loads.staticLoads.Moment::getLoads(), pyNastran.bdf.cards.elements.shell.CTRIA3::getReprDefaults(), pyNastran.bdf.cards.properties.bars.LineProperty::IAreaL(), pyNastran.bdf.cards.dmig.DMI::isComplex(), pyNastran.bdf.cards.dmig.DMI::isReal(), pyNastran.bdf.cards.elements.solid.SolidElement::isSameCard(), pyNastran.bdf.cards.elements.damper.CDAMP1::isSameCard(), pyNastran.bdf.cards.baseCard.BaseCard::isSameFields(), pyNastran.bdf.cards.elements.springs.SpringElement::K(), pyNastran.bdf.cards.elements.mass.CMASS3::Mass(), pyNastran.bdf.cards.properties.bars.PBARL::MassPerLength(), pyNastran.bdf.cards.properties.shell.PCOMP::nPlies(), pyNastran.bdf.cards.baseCard.BaseCard::printCard(), pyNastran.bdf.cards.elements.solid.SolidElement::rawFields(), pyNastran.bdf.cards.elements.elements.CrackElement::rawFields(), pyNastran.bdf.cards.baseCard.BaseCard::reprFields(), pyNastran.bdf.cards.baseCard.BaseCard::writeCodeAster(), and pyNastran.bdf.cards.baseCard.BaseCard::writeCodeAsterLoad().
Trim set identification number.
(Integer > 0)
Definition at line 1265 of file aero.py.
Referenced by pyNastran.bdf.cards.thermal.loads.TEMP::__init__(), pyNastran.bdf.cards.sets.QSET1::__init__(), pyNastran.bdf.cards.methods.EIGR::__init__(), pyNastran.bdf.cards.loads.loads.DLOAD::__init__(), pyNastran.bdf.cards.loads.loads.TabularLoad::__init__(), pyNastran.bdf.cards.loads.loads.RandomLoad::__init__(), pyNastran.bdf.cards.dynamic.FREQ::addFrequencyObject(), pyNastran.bdf.cards.loads.staticLoads.FORCE::Cid(), pyNastran.bdf.cards.thermal.loads.TEMP::crossReference(), pyNastran.bdf.cards.methods.EIGR::crossReference(), pyNastran.bdf.cards.loads.loads.RFORCE::crossReference(), pyNastran.bdf.cards.loads.loads.RLOAD2::crossReference(), pyNastran.bdf.cards.loads.staticLoads.MOMENT1::crossReference(), pyNastran.bdf.cards.loads.staticLoads.MOMENT2::crossReference(), pyNastran.bdf.cards.loads.staticLoads.PLOAD4::crossReference(), pyNastran.bdf.cards.loads.staticLoads.FORCE::F(), pyNastran.bdf.cards.loads.staticLoads.FORCE1::G1(), pyNastran.bdf.cards.loads.loads.RANDPS::getLoads(), pyNastran.bdf.cards.loads.staticLoads.PLOAD::getLoads(), pyNastran.bdf.cards.loads.staticLoads.PLOAD1::getLoads(), pyNastran.bdf.cards.loads.staticLoads.GRAV::GravityVector(), pyNastran.bdf.cards.sets.SET3::IsGrid(), pyNastran.bdf.cards.sets.SET3::IsPoint(), pyNastran.bdf.cards.loads.staticLoads.Moment::M(), pyNastran.bdf.cards.loads.loads.SLOAD::Nid(), pyNastran.bdf.cards.loads.staticLoads.ACCEL1::nodeIDs(), pyNastran.bdf.cards.loads.staticLoads.LOAD::organizeLoads(), pyNastran.bdf.cards.properties.mass.NSM::rawFields(), pyNastran.bdf.cards.thermal.loads.QBDY1::rawFields(), pyNastran.bdf.cards.dynamic.FREQ::rawFields(), pyNastran.bdf.cards.thermal.loads.QBDY3::rawFields(), pyNastran.bdf.cards.sets.SET1::rawFields(), pyNastran.bdf.cards.methods.EIGR::rawFields(), pyNastran.bdf.cards.loads.loads.TLOAD1::rawFields(), pyNastran.bdf.cards.methods.EIGRL::rawFields(), pyNastran.bdf.cards.loads.loads.RFORCE::rawFields(), pyNastran.bdf.cards.loads.staticLoads.FORCE2::rawFields(), pyNastran.bdf.cards.loads.staticLoads.MOMENT::rawFields(), pyNastran.bdf.cards.loads.staticLoads.PLOAD4::rawFields(), pyNastran.bdf.cards.thermal.loads.QBDY1::reprFields(), pyNastran.bdf.cards.methods.EIGB::reprFields(), pyNastran.bdf.cards.dynamic.FREQ4::reprFields(), pyNastran.bdf.cards.thermal.loads.QBDY3::reprFields(), pyNastran.bdf.cards.dynamic.TSTEP::reprFields(), pyNastran.bdf.cards.dynamic.TSTEPNL::reprFields(), pyNastran.bdf.cards.loads.loads.DLOAD::reprFields(), pyNastran.bdf.cards.loads.staticLoads.GRAV::reprFields(), pyNastran.bdf.cards.aero.AEROS::reprFields(), pyNastran.bdf.cards.loads.loads.TLOAD1::reprFields(), pyNastran.bdf.cards.loads.loads.TLOAD2::reprFields(), pyNastran.bdf.cards.loads.loads.RFORCE::reprFields(), pyNastran.bdf.cards.loads.staticLoads.FORCE::reprFields(), pyNastran.bdf.cards.loads.loads.RLOAD1::reprFields(), pyNastran.bdf.cards.loads.staticLoads.FORCE1::reprFields(), pyNastran.bdf.cards.loads.staticLoads.MOMENT1::reprFields(), pyNastran.bdf.cards.loads.staticLoads.PLOAD4::reprFields(), pyNastran.bdf.cards.aero.SPLINE5::Set(), pyNastran.bdf.cards.loads.loads.RLOAD2::Tb(), pyNastran.bdf.cards.loads.loads.RLOAD1::Tc(), pyNastran.bdf.cards.loads.loads.RLOAD1::Td(), pyNastran.bdf.cards.loads.loads.TLOAD1::Tid(), and pyNastran.bdf.cards.loads.loads.RLOAD2::Tp().
Mach number.
(Real > 0.0 and != 1.0)
Definition at line 1266 of file aero.py.
Referenced by pyNastran.bdf.cards.aero.FLFACT.__repr__(), pyNastran::converters::panair::panairWrite::PanairWrite.printGridSummary(), and pyNastran.bdf.cards.aero.SPLINE5.Set().
Dynamic pressure.
(Real > 0.0)
Definition at line 1267 of file aero.py.
Referenced by pyNastran.bdf.cards.aero.SPLINE5.crossReference().
The label identifying aerodynamic trim variables defined on an AESTAT or AESURF entry.
Definition at line 1269 of file aero.py.
Referenced by pyNastran.bdf.cards.aero.SPLINE5.crossReference().
The magnitude of the aerodynamic extra point degree-of-freedom.
(Real)
Definition at line 1271 of file aero.py.
Referenced by pyNastran.bdf.cards.aero.SPLINE5.rawFields().
Flag to request a rigid trim analysis (Real > 0.0 and < 1.0; Default =1.0.
A value of 0.0 provides a rigid trim analysis, not supported
Definition at line 1274 of file aero.py.
Referenced by pyNastran.bdf.cards.aero.SPLINE5.reprFields().