zona
Module
digraph inheritance3d0ba4a332 {
bgcolor=transparent;
rankdir=LR;
size="";
"pyNastran.bdf.cards.aero.aero.Spline" [URL="pyNastran.bdf.cards.aero.aero.html#pyNastran.bdf.cards.aero.aero.Spline",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top"];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.aero.aero.Spline" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.dynamic_loads.Aero" [URL="pyNastran.bdf.cards.aero.dynamic_loads.html#pyNastran.bdf.cards.aero.dynamic_loads.Aero",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Base class for AERO and AEROS cards."];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.aero.dynamic_loads.Aero" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.ACOORD" [URL="#pyNastran.bdf.cards.aero.zona.ACOORD",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines a general coordinate system using three rotational angles as"];
"pyNastran.bdf.cards.coordinate_systems.Coord" -> "pyNastran.bdf.cards.aero.zona.ACOORD" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.AEROZ" [URL="#pyNastran.bdf.cards.aero.zona.AEROZ",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Gives basic aerodynamic parameters for unsteady aerodynamics."];
"pyNastran.bdf.cards.aero.dynamic_loads.Aero" -> "pyNastran.bdf.cards.aero.zona.AEROZ" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.AESURFZ" [URL="#pyNastran.bdf.cards.aero.zona.AESURFZ",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Specifies an aerodynamic control surface for aeroservoelastic, static"];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.aero.zona.AESURFZ" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.BODY7" [URL="#pyNastran.bdf.cards.aero.zona.BODY7",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines an aerodynamic body macroelement of a body-like component."];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.aero.zona.BODY7" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.CAERO7" [URL="#pyNastran.bdf.cards.aero.zona.CAERO7",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Totally wrong..."];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.aero.zona.CAERO7" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.FLUTTER_ZONA" [URL="#pyNastran.bdf.cards.aero.zona.FLUTTER_ZONA",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines data needed to perform flutter, ASE, or a transient response analysis."];
"pyNastran.bdf.cards.aero.aero.Spline" -> "pyNastran.bdf.cards.aero.zona.FLUTTER_ZONA" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.MKAEROZ" [URL="#pyNastran.bdf.cards.aero.zona.MKAEROZ",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top"];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.aero.zona.MKAEROZ" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.PAFOIL7" [URL="#pyNastran.bdf.cards.aero.zona.PAFOIL7",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines an aerodynamic body macroelement of a body-like component."];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.aero.zona.PAFOIL7" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.PANLST1" [URL="#pyNastran.bdf.cards.aero.zona.PANLST1",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines a set of aerodynamic boxes by the LABEL entry in CAERO7 or BODY7"];
"pyNastran.bdf.cards.aero.aero.Spline" -> "pyNastran.bdf.cards.aero.zona.PANLST1" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.PANLST3" [URL="#pyNastran.bdf.cards.aero.zona.PANLST3",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines a set of aerodynamic boxes by the LABEL entry in CAERO7 or BODY7"];
"pyNastran.bdf.cards.aero.aero.Spline" -> "pyNastran.bdf.cards.aero.zona.PANLST3" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.SEGMESH" [URL="#pyNastran.bdf.cards.aero.zona.SEGMESH",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines a grid system for a body segment; referenced by the BODY7 bulk data card."];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.aero.zona.SEGMESH" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.SPLINE1_ZONA" [URL="#pyNastran.bdf.cards.aero.zona.SPLINE1_ZONA",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines an infinite plate spline method for displacements and loads"];
"pyNastran.bdf.cards.aero.aero.Spline" -> "pyNastran.bdf.cards.aero.zona.SPLINE1_ZONA" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.SPLINE2_ZONA" [URL="#pyNastran.bdf.cards.aero.zona.SPLINE2_ZONA",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines an infinite plate spline method for displacements and loads"];
"pyNastran.bdf.cards.aero.aero.Spline" -> "pyNastran.bdf.cards.aero.zona.SPLINE2_ZONA" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.SPLINE3_ZONA" [URL="#pyNastran.bdf.cards.aero.zona.SPLINE3_ZONA",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines a 3-D spline for the BODY7 and CAERO7 macroelement."];
"pyNastran.bdf.cards.aero.aero.Spline" -> "pyNastran.bdf.cards.aero.zona.SPLINE3_ZONA" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.TRIMLNK" [URL="#pyNastran.bdf.cards.aero.zona.TRIMLNK",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines a set of coefficient and trim variable identification"];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.aero.zona.TRIMLNK" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.TRIMVAR" [URL="#pyNastran.bdf.cards.aero.zona.TRIMVAR",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Specifies a trim variable for static aeroelastic trim variables."];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.aero.zona.TRIMVAR" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.TRIM_ZONA" [URL="#pyNastran.bdf.cards.aero.zona.TRIM_ZONA",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Specifies constraints for aeroelastic trim variables."];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.aero.zona.TRIM_ZONA" [arrowsize=0.5,style="setlinewidth(0.5)"];
"pyNastran.bdf.cards.aero.zona.ZONA" [URL="#pyNastran.bdf.cards.aero.zona.ZONA",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top"];
"pyNastran.bdf.cards.base_card.BaseCard" [URL="../pyNastran.bdf.cards.base_card.html#pyNastran.bdf.cards.base_card.BaseCard",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top",tooltip="Defines a series of base methods for every card class"];
"pyNastran.bdf.cards.coordinate_systems.Coord" [URL="../pyNastran.bdf.cards.coordinate_systems.html#pyNastran.bdf.cards.coordinate_systems.Coord",fillcolor=white,fontname="Vera Sans, DejaVu Sans, Liberation Sans, Arial, Helvetica, sans",fontsize=10,height=0.25,shape=box,style="setlinewidth(0.5),filled",target="_top"];
"pyNastran.bdf.cards.base_card.BaseCard" -> "pyNastran.bdf.cards.coordinate_systems.Coord" [arrowsize=0.5,style="setlinewidth(0.5)"];
}
- All ZONA aero cards are defined in this file. This includes:
TRIM
All cards are BaseCard objects.
- class pyNastran.bdf.cards.aero.zona.ACOORD(cid, origin, delta, theta, comment='')[source]
Bases:
Coord
Defines a general coordinate system using three rotational angles as functions of coordinate values in the reference coordinate system. The CORD3G entry is used with the MAT9 entry to orient material principal axes for 3-D composite analysis.
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ACOORD
ID
XORIGN
YORIGN
ZORIGN
DELTA
THETA
ACOORD
10
250.0
52.5
15.0
0.0
0.0
Defines the CORD3G card
- Parameters:
- cidint
coordinate system id
- originlist[float]
the xyz origin
- deltafloat
pitch angle
- thetafloat
roll angle
- commentstr; default=’’
a comment for the card
- Type = 'R'
- acoord_transform_to_global(p)[source]
- Parameters:
- p(3,) float ndarray
the point to transform
- .. warning:: not done, just setting up how you’d do this
- .. note:: per http://en.wikipedia.org/wiki/Euler_angles
“This means for example that a convention named (YXZ) is the result of performing first an intrinsic Z rotation, followed by X and Y rotations, in the moving axes (Note: the order of multiplication of matrices is the opposite of the order in which they’re applied to a vector).”
- classmethod add_card(card, comment='')[source]
Adds a ACOORD card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- cross_reference(model: BDF) None [source]
Cross links the card so referenced cards can be extracted directly
- Parameters:
- modelBDF()
the BDF object
- property rid
- setup()[source]
- \[e_{13} = e_3 - e_1\]\[e_{12} = e_2 - e_1\]\[k = \frac{e_{12}}{\lvert e_{12} \rvert}\]\[j_{dir} = k \times e_{13}\]\[j = \frac{j_{dir}}{\lvert j_{dir} \rvert}\]\[i = j \times k\]
- type = 'ACOORD'
- class pyNastran.bdf.cards.aero.zona.AEROZ(fm_mass_unit, fm_length_unit, cref, bref, sref, flip='NO', acsid=0, rcsid=0, sym_xz=0, xyz_ref=None, comment='')[source]
Bases:
Aero
Gives basic aerodynamic parameters for unsteady aerodynamics.
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8
AEROS
ACSID
RCSID
REFC
REFB
REFS
SYMXZ
SYMXY
AEROS
10
20
1
Creates an AEROZ card
- Parameters:
- creffloat
the aerodynamic chord
- breffloat
the wing span for a half model, this should be the full span for a full model, this should be the full span
- sreffloat
the wing area for a half model, this should be the half area for a full model, this should be the full area
- acsidint; default=0
aerodyanmic coordinate system defines the direction of the wind
- rcsidint; default=0
coordinate system for rigid body motions
- sym_xzint; default=0
xz symmetry flag (+1=symmetry; -1=antisymmetric)
- commentstr; default=’’
a comment for the card
- acsid
Aerodynamic coordinate system identification.
- classmethod add_card(card, comment='')[source]
Adds an AEROZ card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- $ ACSID XZSYM FLIP FMMUNIT FMLUNIT REFC REFB REFS
- $+ABC REFX REFY REFZ
- AEROZ 0 YES NO SLIN IN 22.73 59.394 1175.8
59.53 0.0 0.0
- bref
Reference span
- cref
Reference chord length
- cross_reference(model: BDF) None [source]
Cross reference aerodynamic coordinate system.
- Parameters:
- modelBDF
The BDF object.
- raw_fields()[source]
Gets the fields in their unmodified form
- Returns:
- fieldslist[varies]
the fields that define the card
- rcsid
Reference coordinate system identification for rigid body motions.
- repr_fields()[source]
Gets the fields in their simplified form
- Returns:
- fieldslist[varies]
the fields that define the card
- safe_cross_reference(model: BDF, xref_errors)[source]
Safe cross reference aerodynamic coordinate system.
- Parameters:
- modelBDF
The BDF object.
- sref
Reference wing area
- sym_xz
Symmetry key for the aero coordinate x-z plane. See Remark 6. (Integer = +1 for symmetry, 0 for no symmetry, and -1 for antisymmetry; Default = 0)
- type = 'AEROZ'
- class pyNastran.bdf.cards.aero.zona.AESURFZ(label, surface_type, cid, panlst, setg, actuator_tf, comment='')[source]
Bases:
BaseCard
Specifies an aerodynamic control surface for aeroservoelastic, static aeroelastic/trim analysis, or the transient response analysis.
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AESURFZ
LABEL
TYPE
CID
SETK
SETG
ACTID
AESURFZ
RUDDER
ASYM
1
10
20
0
Creates an AESURF card, which defines a control surface
- Parameters:
- labelstr
controller name
- surface_typestr
defines the control surface type {SYM, ASYM}
- cidint
coordinate system id to define the hinge axis
- panlstint
aero panels defined by PANLST
- setgint
???
- actuator_tfint
???
- commentstr; default=’’
a comment for the card
- classmethod add_card(card, comment='')[source]
Adds an AESURF card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- property aesid
- property alid1_ref
- cid
Identification number of a rectangular coordinate system with a y-axis that defines the hinge line of the control surface component.
- convert_to_nastran(model, aesurf_id, aelist_id)[source]
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AESURF
ID
LABEL
CID1
ALID1
CID2
ALID2
EFF
LDW
CREFC
CREFS
PLLIM
PULIM
HMLLIM
HMULIM
TQLLIM
TQULIM
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2
3
4
5
6
7
AESURFZ
LABEL
TYPE
CID
SETK
SETG
ACTID
AESURFZ
RUDDER
ASYM
1
10
20
0
- cross_reference(model: BDF) None [source]
Cross links the card so referenced cards can be extracted directly
- Parameters:
- modelBDF()
the BDF object
- label
Controller name.
- raw_fields()[source]
Gets the fields in their unmodified form
- Returns:
- fieldsreset_camera[int/float/str]
the fields that define the card
- repr_fields()[source]
Gets the fields in their simplified form
- Returns:
- fieldslist[int/float/str]
the fields that define the card
- type = 'AESURFZ'
- class pyNastran.bdf.cards.aero.zona.BODY7(eid, label, pid, nseg, idmeshes, acoord=0, comment='')[source]
Bases:
BaseCard
Defines an aerodynamic body macroelement of a body-like component. Similar to Nastran’s CAERO2.
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7
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9
CAERO2
EID
PID
CP
NSB
NINT
LSB
LINT
IGID
X1
Y1
Z1
X12
1
2
3
4
5
6
7
8
9
BODY7
BID
LABEL
IPBODY7
ACOORD
NSEG
IDMESH1
IDMESH2
IDMESH3
IDMESH4
etc
BODY7
4
BODY
2
8
4
20
21
22
23
Defines a BODY7 card, which defines a slender body (e.g., fuselage/wingtip tank).
- Parameters:
- eidint
body id
- labelstr
An arbitrary character string used to define the body.
- pidint; default=0
Identification number of PBODY7 bulk data card (specifying body wake and/or inlet aerodynamic boxes)
- acoordint; default=0
Identification number of ACOORD bulk data card (specifying body center line location and orientation)
- nsegint
Number of body segments
- idmesheslist[int]
Identification number of SEGMESH bulk data card (specifying body segments).
- commentstr; default=’’
a comment for the card
- _get_body7_width_height_radius(thetas: ndarray, itype: int, camber: float, yrad: float, zrad: float, idy_ref, idz_ref) tuple[float, float, float, float, float] [source]
- _get_points_elements_3di(segmesh: SEGMESH) tuple[ndarray, ndarray] [source]
- points (nchord, nspan) float ndarray; might be backwards???
the points
- elements (nquads, 4) int ndarray
series of quad elements nquads = (nchord-1) * (nspan-1)
- _get_xyzs_offset(origin_x, origin_y, origin_z, thetas, itype: int, x: float, yrad: float, zrad: float, camber: float, idy_ref, idz_ref) tuple[list[float], ndarray, ndarray] [source]
- classmethod add_card(card, comment='')[source]
Adds a BODY7 card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- convert_to_nastran(model)[source]
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CAERO2
EID
PID
CP
NSB
NINT
LSB
LINT
IGID
X1
Y1
Z1
X12
1
2
3
4
5
6
7
8
9
BODY7
BID
LABEL
IPBODY7
ACOORD
NSEG
IDMESH1
IDMESH2
IDMESH3
IDMESH4
etc
BODY7
4
BODY
2
8
4
20
21
22
23
- cross_reference(model: BDF) None [source]
Cross links the card so referenced cards can be extracted directly
- Parameters:
- modelBDF()
the BDF object
- eid
Element identification number
- get_points_elements_3d()[source]
Gets the points/elements in 3d space as CQUAD4s The idea is that this is used by the GUI to display CAERO panels.
TODO: doesn’t support the aero coordinate system
- property nboxes
- property npanels: int
gets the number of panels for the body
- pid
Property identification number of a PAERO7 entry.
- raw_fields() list[Any] [source]
Gets the fields in their unmodified form
- Returns:
- fieldslist
The fields that define the card
- repr_fields() list[Any] [source]
Gets the fields in their simplified form
- Returns:
- fieldslist
The fields that define the card
- type = 'BODY7'
- class pyNastran.bdf.cards.aero.zona.CAERO7(eid, label, p1, x12, p4, x43, cp=0, nspan=0, nchord=0, lspan=0, p_airfoil=None, ztaic=None, comment='')[source]
Bases:
BaseCard
Totally wrong…
Defines an aerodynamic macro element (panel) in terms of two leading edge locations and side chords. This is used for Doublet-Lattice theory for subsonic aerodynamics and the ZONA51 theory for supersonic aerodynamics.
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CAERO7
WID
LABEL
ACOORD
NSPAN
NCHORD
LSPAN
ZTAIC
PAFOIL7
XRL
YRL
ZRL
RCH
LRCHD
ATTCHR
ACORDR
XTL
YTL
ZTL
TCH
LTCHD
ATTCHT
ACORDT
1 | | | | 4 | | | | 2------3
- Attributes:
- eidint
element id
- pidint, PAERO1
int : PAERO1 ID PAERO1 : PAERO1 object (xref)
- igidint
Group number
- p1(1, 3) ndarray float
xyz location of point 1 (leading edge; inboard)
- p4(1, 3) ndarray float
xyz location of point 4 (leading edge; outboard)
- x12float
distance along the flow direction from node 1 to node 2; (typically x, root chord)
- x43float
distance along the flow direction from node 4 to node 3; (typically x, tip chord)
- cpint, CORDx
int : coordinate system CORDx : Coordinate object (xref)
- nspanint
int > 0 : N spanwise boxes distributed evenly int = 0 : use lchord
- nchordint
int > 0 : N chordwise boxes distributed evenly int = 0 : use lchord
- lspanint, AEFACT
int > 0 : AEFACT reference for non-uniform nspan int = 0 : use nspan AEFACT : AEFACT object (xref)
- lchordint, AEFACT
int > 0 : AEFACT reference for non-uniform nchord int = 0 : use nchord AEFACT : AEFACT object (xref)
comment
str; default=’’accesses the comment
Defines a CAERO1 card, which defines a simplified lifting surface (e.g., wing/tail).
- Parameters:
- eidint
element id
- pidint, PAERO1
int : PAERO1 ID PAERO1 : PAERO1 object (xref)
- igroupint
Group number
- p1(1, 3) ndarray float
xyz location of point 1 (leading edge; inboard)
- p4(1, 3) ndarray float
xyz location of point 4 (leading edge; outboard)
- x12float
distance along the flow direction from node 1 to node 2; (typically x, root chord)
- x43float
distance along the flow direction from node 4 to node 3; (typically x, tip chord)
- cpint, CORDx; default=0
int : coordinate system CORDx : Coordinate object (xref)
- nspanint; default=0
int > 0 : N spanwise boxes distributed evenly int = 0 : use lchord
- nchordint; default=0
int > 0 : N chordwise boxes distributed evenly int = 0 : use lchord
- lspanint, AEFACT; default=0
int > 0 : AEFACT reference for non-uniform nspan int = 0 : use nspan AEFACT : AEFACT object (xref)
- lchordint, AEFACT; default=0
int > 0 : AEFACT reference for non-uniform nchord int = 0 : use nchord AEFACT : AEFACT object (xref)
- commentstr; default=’’
a comment for the card
- _get_box_x_chord_center(box_id, x_chord)[source]
The the location of the x_chord of the box along the centerline.
- classmethod add_card(card, comment='')[source]
Adds a CAERO7 card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- CAERO7 100101 RIBW1 2 25
998.904 39.821 230.687 1298.159 310001 1121.821 61.134 236.560 1175.243
- CAERO7 100201 RIBW2 2 25
1121.821 61.134 236.560 1175.243 1244.258 84.704 243.625 1052.805
- convert_to_nastran()[source]
1
2
3
4
5
6
7
8
9
CAERO1
EID
PID
CP
NSPAN
NCHORD
LSPAN
LCHORD
IGID
X1
Y1
Z1
X12
X4
Y4
Z4
X43
- cp
Coordinate system for locating point 1.
- cross_reference(model: BDF) None [source]
Cross links the card so referenced cards can be extracted directly
- Parameters:
- modelBDF()
the BDF object
- eid
Element identification number
- get_box_index(box_id)[source]
Get the index of
self.box_ids
that corresponds to the given box id.- Parameters:
- box_idint
Box id to get the index of.
- Returns:
- indextuple
Index of
self.box_ids
that corresponds to the given box id.
- get_box_mid_chord_center(box_id)[source]
The the location of the mid chord of the box along the centerline.
- Parameters:
- box_idint
Box id.
- Returns:
- xyz_mid_chordndarray
Location of box mid chord in global.
- get_box_quarter_chord_center(box_id)[source]
The the location of the quarter chord of the box along the centerline.
- Parameters:
- box_idint
Box id.
- Returns:
- xyz_quarter_chordndarray
Location of box quarter chord in global.
- get_npanel_points_elements()[source]
Gets the number of sub-points and sub-elements for the CAERO card
- Returns:
- npointsint
The number of nodes for the CAERO
- nelmementsint
The number of elements for the CAERO
- get_points()[source]
Get the 4 corner points for the CAERO card
- Returns:
- p1234(4, 3) list
List of 4 corner points in the global frame
- label
Property identification number of a PAERO2 entry.
- property min_max_eid
Gets the min and max element ids of the CAERO card
- Returns:
- min_max_eid(2, ) list
The [min_eid, max_eid]
- property npanels
- panel_points_elements()[source]
Gets the sub-points and sub-elements for the CAERO card
- Returns:
- points(nnodes,3) ndarray of floats
the array of points
- elements(nelements,4) ndarray of integers
the array of point ids
- raw_fields()[source]
Gets the fields in their unmodified form
- Returns:
- fieldslist
the fields that define the card
- repr_fields()[source]
Gets the fields in their simplified form
- Returns:
- fieldsLIST
The fields that define the card
- safe_cross_reference(model: BDF, xref_errors)[source]
Cross links the card so referenced cards can be extracted directly
- Parameters:
- modelBDF()
the BDF object
- property shape
returns (nelements_nchord, nelements_span)
- type = 'CAERO7'
- write_card(size: int = 8, is_double: bool = False) str [source]
Writes the card with the specified width and precision
- Parameters:
- sizeint (default=8)
size of the field; {8, 16}
- is_doublebool (default=False)
is this card double precision
- Returns:
- msgstr
the string representation of the card
- property xy
- Returns:
- x(nchord,) ndarray
The percentage x location in the chord-wise direction of each panel
- y(nspan,) ndarray
The percentage y location in the span-wise direction of each panel
- class pyNastran.bdf.cards.aero.zona.FLUTTER_ZONA(sid, sym, fix, nmode, tabdmp, mlist, conmlst, nkstep=25, comment='')[source]
Bases:
Spline
Defines data needed to perform flutter, ASE, or a transient response analysis.
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2
3
4
5
6
7
8
9
FLUTTER
SID
METHOD
DENS
MACH
RFREQ
IMETH
NVALUE/OMAX
EPS
FLUTTER
19
K
119
219
319
S
5
1.-4
1
2
3
4
5
6
7
8
9
FLUTTER
SETID
SYM
FIX
NMODE
TABDMP
MLIST
CONMLST
NKSTEP
FLUTTER
100
SYMM3
1
0
30
100
0
50
Creates a FLUTTER card, which is required for a flutter (SOL 145) analysis.
- Parameters:
- sidint
Unique set identification number. (Integer > 0)
- symstr
Character string up to 8 characters with no embedded blanks. The first 4 characters can be either ‘SYMM’ (or ‘SYM’), ‘ANTI’, or ‘ASYM’ that defines the boundary condition of the structural finite element model as well as the unsteady aerodynamics, where:
SYMM Symmetric boundary condition.
ANTI Antisymmetric boundary condition.
ASYM Asymmetric boundary condition.
The last 4 characters are used to specify the interpolation scheme for the generalized aerodynamic matrices. They can be either:
blank for a cubic spline
L for a linear interpolation. (such as SYM = ‘SYMML’, ‘ANTIL’, or ‘ASYML’)
P for a second-order-polynomial interpolation. (such as SYM = ‘SYMMP’, ‘ANTIP’, or ‘ASYMP’)
integer for a hybrid cubic spline and linear interpolation scheme. (such as SYM = ‘SYMM1’, ‘SYMM2’, ‘ANTI3’, etc.)
(Default = SYMML)
- fixint
Identification number of a FIXHATM, FIXMATM, FIXMACH, or FIXMDEN bulk data card. (Integer > 0)
- nmodeint
Number of structural modes used in the flutter analysis. (Integer >= 0)
- tabdmpint
Identification number of a TABDMP1 bulk data card specifying modal damping as
a function of natural frequency. (Integer ≥ 0)
- mlistint
Identification number of a SET1 or SETADD bulk data card specifying a list of normal modes to be omitted from the flutter analysis. (Integer >= 0)
- conmlstint
Identification number of a CONMLST bulk data card specifying a list of identification numbers of the CONM1 bulk data cards for mass perturbation. (Integer >= 0) (See Remark 8)
- nkstepint; default=25
Number of reduced frequency steps for the reduced-frequency-sweep technique of the g-Method flutter solution. (Integer >= 0)
- classmethod add_card(card, comment='')[source]
Adds a FLUTTER card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- type = 'FLUTTER_ZONA'
- class pyNastran.bdf.cards.aero.zona.MKAEROZ(sid, mach, flt_id, filename, print_flag, freqs, method=0, save=None, comment='')[source]
Bases:
BaseCard
- Parameters:
- sidint
the MKAEROZ id
- machfloat
the mach number for the TRIM solution
- savestr
save the AIC data to the filename SAVE save the AICs ACQUIRE load an AIC database ADD append the new acids to the existing AIC database RESTART continue an analysis
- filenamestr
the length of the file must be at most 56 characters
- print_flagint
???
- freqslist[float]
???
- methodint
???
- save???
???
- commentstr; default=’’
a comment for the card
- repr_fields()[source]
Gets the fields in their simplified form
- Returns:
- fieldslist[varies]
the fields that define the card
- type = 'MKAEROZ'
- class pyNastran.bdf.cards.aero.zona.PAFOIL7(pid, i_axial, i_thickness_root, i_camber_root, le_radius_root, i_thickness_tip, i_camber_tip, le_radius_tip, comment='')[source]
Bases:
BaseCard
Defines an aerodynamic body macroelement of a body-like component. Similar to Nastran’s CAERO2.
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2
3
4
5
6
7
8
9
PAFOIL7
ID
ITAX
ITHR
ICAMR
RADR
ITHT
ICAMT
RADT
PAFOIL7
1
-201
202
203
0.1
211
212
0.1
Defines a BODY7 card, which defines a slender body (e.g., fuselage/wingtip tank).
- Parameters:
- pidint
PAFOIL7 identification number.
- i_axialstr
Identification number of an AEFACT bulk data card used to specify the xcoordinate locations, in percentage of the chord length, where the thickness and camber are specified. ITAX can be a negative number (where ABS (ITAX) = AEFACT bulk data card identification number) to request linear interpolation.
- i_thickness_root / i_thickness_tipint
Identification number of an AEFACT bulk data card used to specify the half thickness of the airfoil at the wing root/tip.
- i_camberint; default=0
Identification number of an AEFACT bulk data card used to specify the camber of the airfoil at the wing root.
- le_radius_root / le_radius_root: float
Leading edge radius at the root/tip normalized by the root/tip chord.
- i_thickness_tipint
Identification number of an AEFACT bulk data card used to specify the half thickness at the wing tip.
- commentstr; default=’’
a comment for the card
- classmethod add_card(card, comment='')[source]
Adds a PAFOIL7 card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- convert_to_nastran(model)[source]
Should this be converted to a DMIG?
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2
3
4
5
6
7
8
9
PAFOIL7
ID
ITAX
ITHR
ICAMR
RADR
ITHT
ICAMT
RADT
PAFOIL7
1
-201
202
203
0.1
211
212
0.1
- cross_reference(model: BDF) None [source]
Cross links the card so referenced cards can be extracted directly
- Parameters:
- modelBDF()
the BDF object
- raw_fields()[source]
Gets the fields in their unmodified form
- Returns:
- fieldslist
The fields that define the card
- repr_fields()[source]
Gets the fields in their simplified form
- Returns:
- fieldslist
The fields that define the card
- type = 'PAFOIL7'
- class pyNastran.bdf.cards.aero.zona.PANLST1(eid, macro_id, box1, box2, comment='')[source]
Bases:
Spline
Defines a set of aerodynamic boxes by the LABEL entry in CAERO7 or BODY7 bulk data cards.
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2
3
4
5
6
7
8
9
SPLINE1
EID
MODEL
CP
SETK
SETG
DZ
EPS
SPLINE1
100
1
10
1
2
3
4
5
6
7
8
9
PANLST1
SETID
MACROID
BOX1
BOX2
PANLST1
100
111
111
118
PANLST1 is referred to by SPLINEi, ATTACH, LOADMOD, CPFACT, JETFRC, and/or AESURFZ bulk data card.
Creates a PANLST1 card
- Parameters:
- eidint
spline id
- commentstr; default=’’
a comment for the card
- classmethod add_card(card, comment='')[source]
Adds a PANLST3 card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- type = 'PANLST1'
- class pyNastran.bdf.cards.aero.zona.PANLST3(eid, panel_groups, comment='')[source]
Bases:
Spline
Defines a set of aerodynamic boxes by the LABEL entry in CAERO7 or BODY7 bulk data cards.
1
2
3
4
5
6
7
8
9
SPLINE1
EID
MODEL
CP
SETK
SETG
DZ
EPS
SPLINE1
100
1
10
1
2
3
4
5
6
7
8
9
PANLST3
SETID
LABEL1
LABEL2
LABEL3
etc
PANLST3
100
WING
HTAIL
PANLST3 is referred to by SPLINEi, ATTACH, LOADMOD, CPFACT, JETFRC, and/or AESURFZ bulk data card.
Creates a PANLST3 card
- Parameters:
- eidint
spline id
- commentstr; default=’’
a comment for the card
- classmethod add_card(card, comment='')[source]
Adds a PANLST3 card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- type = 'PANLST3'
- class pyNastran.bdf.cards.aero.zona.SEGMESH(segmesh_id, naxial, nradial, nose_radius, iaxis, itypes, xs, cambers, ys, zs, idys, idzs, comment='')[source]
Bases:
BaseCard
Defines a grid system for a body segment; referenced by the BODY7 bulk data card.
1
2
3
4
5
6
7
8
9
SEGMESH
IDMESH
NAXIS
NRAD
NOSERAD
IAXIS
ITYPE1
X1
CAM1
YR1
ZR1
IDY1
IDZ1
ITYPE2
X2
CAM2
YR2
ZR2
IDY2
IDZ2
ITYPE3
X3
CAM3
YR3
ZR3
IDY3
IDZ3
SEGMESH
2
3
6
1
0.0
0.0
0.0
1
1.0
0.0
0.5
3
2.0
103
104
Defines a SEGMESH card, which defines a cross-section for a PBODY7.
- Parameters:
- segmesh_idint
Body segment mesh identification number.
- naxialint
Number of axial stations (i.e., divisions) of the segment. (min=2).
- nradialint
Number of circumferential points of the segment (min=3).
- nose_radiusfloat
Nose radius of blunt body. NOSERAD is active only if ZONA7U (Hypersonic Aerodynamic Method) is used (the METHOD entry of the MKAEROZ Bulk Data equals 2 or –2). Furthermore, NOSERAD is used only if the SEGMESH bulk data card is the first segment defined in the BODY7 bulk data card.
- iaxisint
The index of the axial station where the blunt nose ends. IAXIS is active only if ZONA7U (Hypersonic Aerodynamic Method) is used.
- ITYPEiint
Type of input used to define the circumferential box cuts - 1 body of revolution - 2 elliptical body - 3 arbitrary body
- Xilist[float]
X-location of the axial station; Xi must be in ascending order. (i.e., Xi+1 > Xi)
- camberslist[float]
Body camber at the Xi axial station. (Real)
- YRilist[float]
Body cross-sectional radius if ITYPEi = 1 or the semi-axis length of the elliptical body parallel to the Y-axis if ITYPEi=2.
- ZRilist[float]
The semi-axis length of the elliptical body parallel to the Z-axis. Used only if ITYPEi=2. (Real)
- IDYiint
Identification number of AEFACT bulk data card that specifies NRAD number of the Y-coordinate locations of the circumferential points at the Xi axial station. Use only if ITYPEi=3.
- IDZiint
Identification number of AEFACT bulk data card that specifies NRAD number of the Z-coordinate locations of the circumferential points at the Xi axial station. Use only if ITYPEi=3.
- commentstr; default=’’
a comment for the card
- classmethod add_card(card, comment='')[source]
Adds a SEGMESH card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- property pid: int
- raw_fields()[source]
Gets the fields in their unmodified form
- Returns:
- fieldslist
The fields that define the card
- repr_fields()[source]
Gets the fields in their simplified form
- Returns:
- fieldslist
The fields that define the card
- type = 'SEGMESH'
- class pyNastran.bdf.cards.aero.zona.SPLINE1_ZONA(eid, panlst, setg, model=None, cp=None, dz=None, eps=0.01, comment='')[source]
Bases:
Spline
Defines an infinite plate spline method for displacements and loads transferal between CAERO7 macroelement and structural grid points.
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2
3
4
5
6
7
8
9
SPLINE1
EID
CAERO
BOX1
BOX2
SETG
DZ
METH
USAGE
NELEM
MELEM
SPLINE1
3
111
115
122
14
1
2
3
4
5
6
7
8
9
SPLINE1
EID
MODEL
CP
SETK
SETG
DZ
EPS
SPLINE1
100
1
10
Creates a SPLINE1 card, which is useful for control surface constraints.
- Parameters:
- eidint
spline id
- commentstr; default=’’
a comment for the card
- classmethod add_card(card, comment='')[source]
Adds a SPLINE1 card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- convert_to_nastran(model)[source]
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2
3
4
5
6
7
8
9
SPLINE1
EID
CAERO
BOX1
BOX2
SETG
DZ
METH
USAGE
NELEM
MELEM
SPLINE1
3
111
115
122
14
1
2
3
4
5
6
7
8
9
SPLINE1
EID
MODEL
CP
SETK
SETG
DZ
EPS
SPLINE1
100
1
10
- type = 'SPLINE1_ZONA'
- class pyNastran.bdf.cards.aero.zona.SPLINE2_ZONA(eid, panlst, setg, model=None, dz=None, eps=0.01, cp=None, curvature=None, comment='')[source]
Bases:
Spline
Defines an infinite plate spline method for displacements and loads transferal between CAERO7 macroelement and structural grid points.
1
2
3
5
6
6
7
8
9
SPLINE2
EID
MODEL
SETK
SETG
DZ
EPS
CP
CURV
SPLINE2
100
1
10
Creates a SPLINE1 card, which is useful for control surface constraints.
- Parameters:
- eidint
spline id
- commentstr; default=’’
a comment for the card
- classmethod add_card(card, comment='')[source]
Adds a SPLINE1 card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- type = 'SPLINE2_ZONA'
- class pyNastran.bdf.cards.aero.zona.SPLINE3_ZONA(eid, panlst, setg, model=None, cp=None, dz=None, eps=0.01, comment='')[source]
Bases:
Spline
Defines a 3-D spline for the BODY7 and CAERO7 macroelement.
1
2
3
4
5
6
7
8
9
SPLINE3
EID
MODEL
CP
SETK
SETG
DZ
EPS
SPLINE3
100
N/A
1
10
Creates a SPLINE3 card, which is useful for control surface constraints.
- Parameters:
- eidint
spline id
- commentstr; default=’’
a comment for the card
- classmethod add_card(card, comment='')[source]
Adds a SPLINE3 card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- raw_fields()[source]
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2
3
4
5
6
7
8
9
SPLINE3
EID
CAERO
BOXID
COMP
G1
C1
A1
USAGE
G2
C2
A2
G3
C3
A2
—
G4
C4
A4
etc.
- type = 'SPLINE3_ZONA'
- class pyNastran.bdf.cards.aero.zona.TRIMLNK(link_id, sym, coeffs, var_ids, comment='')[source]
Bases:
BaseCard
Defines a set of coefficient and trim variable identification number pairs for trim variable linking.
+=========+========+========+========+========+========+========+========+========+ | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9 | +———+——–+——–+——–+——–+——–+——–+——–+——–+ | TRIMLNK | IDLINK | SYM | COEFF1 | IDVAR1 | COEFF2 | IDVAR2 | COEFF3 | IDVAR3 | +———+——–+——–+——–+——–+——–+——–+——–+——–+ | | COEFF4 | IDVAR4 | etc. | | | | | | +———+——–+——–+——–+——–+——–+——–+——–+——–+
Creates a TRIMLNK card
- Parameters:
- link_idint
the TRIMLNK id
- sym???
???
- coeffs???
???
- var_ids???
???
- commentstr; default=’’
a comment for the card
- classmethod add_card(card, comment='')[source]
Adds a TRIMLNK card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- raw_fields()[source]
Gets the fields in their unmodified form
- Returns:
- fieldslist[varies]
the fields that define the card
- repr_fields()[source]
Gets the fields in their simplified form
- Returns:
- fieldslist[varies]
the fields that define the card
- type = 'TRIMLNK'
- class pyNastran.bdf.cards.aero.zona.TRIMVAR(var_id, label, lower, upper, trimlnk, dmi, sym, initial, dcd, dcy, dcl, dcr, dcm, dcn, comment='')[source]
Bases:
BaseCard
Specifies a trim variable for static aeroelastic trim variables.
Creates a TRIMVAR card for a static aero (144) analysis.
- Parameters:
- var_idint
the trim id; referenced by the Case Control TRIM field
- commentstr; default=’’
a comment for the card
- classmethod add_card(card, comment='')[source]
Adds a TRIMVAR card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- raw_fields()[source]
Gets the fields in their unmodified form
- Returns:
- fieldslist[varies]
the fields that define the card
- repr_fields()[source]
Gets the fields in their simplified form
- Returns:
- fieldslist[varies]
the fields that define the card
- type = 'TRIMVAR'
- class pyNastran.bdf.cards.aero.zona.TRIM_ZONA(sid, mkaeroz, q, cg, true_g, nxyz, pqr, loadset, labels, uxs, comment='')[source]
Bases:
BaseCard
Specifies constraints for aeroelastic trim variables.
Creates a TRIM card for a static aero (144) analysis.
- Parameters:
- sidint
the trim id; referenced by the Case Control TRIM field
- qfloat
dynamic pressure
- true_gfloat
???
- nxyzlist[float]
???
- pqrlist[float]
[roll_rate, pitch_rate, yaw_rate]
- loadsetint
Identification number of a SET1 or SETADD bulk data card that specifies a set of identification numbers of TRIMFNC or TRIMADD bulk data card. All values of the trim functions defined by the TRIMFNC or TRIMADD bulk data card are computed and printed out.
- labelslist[str]
names of the fixed variables
- uxslist[float]
values corresponding to labels
- commentstr; default=’’
a comment for the card
- classmethod add_card(card, comment='')[source]
Adds a TRIM card from
BDF.add_card(...)
- Parameters:
- cardBDFCard()
a BDFCard object
- commentstr; default=’’
a comment for the card
- labels
The label identifying aerodynamic trim variables defined on an AESTAT or AESURF entry.
- q
Dynamic pressure. (Real > 0.0)
- raw_fields()[source]
Gets the fields in their unmodified form
- Returns:
- fieldslist[varies]
the fields that define the card
- repr_fields()[source]
Gets the fields in their simplified form
- Returns:
- fieldslist[varies]
the fields that define the card
- sid
Trim set identification number. (Integer > 0)
- type = 'TRIM_ZONA'
- uxs
The magnitude of the aerodynamic extra point degree-of-freedom. (Real)
- class pyNastran.bdf.cards.aero.zona.ZONA(model)[source]
Bases:
object
- _convert_aesurf_aelist()[source]
Converts ZONA AESURFZ to AESURF/AELIST
1
2
3
4
5
6
7
AESURFZ
LABEL
TYPE
CID
SETK
SETG
ACTID
AESURFZ
RUDDER
ASYM
1
10
20
0
- object_attributes(mode: str = 'public', keys_to_skip: list[str] | None = None, filter_properties: bool = False)[source]
List the names of attributes of a class as strings. Returns public attributes as default.
- Parameters:
- modestr
defines what kind of attributes will be listed * ‘public’ - names that do not begin with underscore * ‘private’ - names that begin with single underscore * ‘both’ - private and public * ‘all’ - all attributes that are defined for the object
- keys_to_skiplist[str]; default=None -> []
names to not consider to avoid deprecation warnings
- Returns:
- attribute_nameslist[str]
sorted list of the names of attributes of a given type or None if the mode is wrong
- object_methods(mode: str = 'public', keys_to_skip: list[str] | None = None) list[str] [source]
List the names of methods of a class as strings. Returns public methods as default.
- Parameters:
- objinstance
the object for checking
- modestr
defines what kind of methods will be listed * “public” - names that do not begin with underscore * “private” - names that begin with single underscore * “both” - private and public * “all” - all methods that are defined for the object
- keys_to_skiplist[str]; default=None -> []
names to not consider to avoid deprecation warnings
- Returns:
- methodlist[str]
sorted list of the names of methods of a given type or None if the mode is wrong
- pafoil
store PAFOIL7/PAFOIL8
- panlsts
store PANLST1,PANLST2,PANLST3