pyNastran
0.5.0
pyNastran BDF Reader/Writer, OP2 Parser, and GUI
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Go to the source code of this file.
Classes | |
class | pyNastran.bdf.cards.aero.AEFACT |
Defines real numbers for aeroelastic analysis. More... | |
class | pyNastran.bdf.cards.aero.AELINK |
Defines relationships between or among AESTAT and AESURF entries, such that:
\[ u^D + \Sigma_{i=1}^n C_i u_i^I = 0.0\] AELINK ID LABLD LABL1 C1 LABL2 C2 LABL3 C3 LABL4 C4 -etc. More... | |
class | pyNastran.bdf.cards.aero.AELIST |
Defines a list of aerodynamic elements to undergo the motion prescribed with the AESURF Bulk Data entry for static aeroelasticity. More... | |
class | pyNastran.bdf.cards.aero.AEPARM |
Defines a general aerodynamic trim variable degree-of-freedom (aerodynamic extra point). More... | |
class | pyNastran.bdf.cards.aero.AESTAT |
Specifies rigid body motions to be used as trim variables in static aeroelasticity. More... | |
class | pyNastran.bdf.cards.aero.AESURF |
Specifies an aerodynamic control surface as a member of the set of aerodynamic extra points. More... | |
class | pyNastran.bdf.cards.aero.AESURFS |
Optional specification of the structural nodes associated with an aerodynamic control surface that has been defined on an AESURF entry. More... | |
class | pyNastran.bdf.cards.aero.Aero |
Base class for AERO and AEROS cards. More... | |
class | pyNastran.bdf.cards.aero.AERO |
Gives basic aerodynamic parameters for unsteady aerodynamics. More... | |
class | pyNastran.bdf.cards.aero.AEROS |
Gives basic aerodynamic parameters for unsteady aerodynamics. More... | |
class | pyNastran.bdf.cards.aero.CSSCHD |
Defines a scheduled control surface deflection as a function of Mach number and angle of attack. More... | |
class | pyNastran.bdf.cards.aero.CAERO1 |
Defines an aerodynamic macro element (panel) in terms of two leading edge locations and side chords. More... | |
class | pyNastran.bdf.cards.aero.CAERO2 |
Aerodynamic Body Connection Defines aerodynamic slender body and interference elements for Doublet-Lattice aerodynamics. More... | |
class | pyNastran.bdf.cards.aero.CAERO3 |
class | pyNastran.bdf.cards.aero.CAERO4 |
class | pyNastran.bdf.cards.aero.CAERO5 |
class | pyNastran.bdf.cards.aero.FLFACT |
FLFACT SID F1 F2 F3 F4 F5 F6 F7 F8 F9 -etc. More... | |
class | pyNastran.bdf.cards.aero.FLUTTER |
Defines data needed to perform flutter analysis. More... | |
class | pyNastran.bdf.cards.aero.GUST |
Defines a stationary vertical gust for use in aeroelastic response analysis. More... | |
class | pyNastran.bdf.cards.aero.MKAERO1 |
Provides a table of Mach numbers (m) and reduced frequencies (k) for aerodynamic matrix calculation MKAERO1 m1 m2 m3 m4 m5 m6 m7 m8 k1 k2 k3 k4 k5 k6 k7 k8. More... | |
class | pyNastran.bdf.cards.aero.MKAERO2 |
Provides a table of Mach numbers (m) and reduced frequencies (k) for aerodynamic matrix calculation MKAERO2 m1 k1 m2 k2 m3 k3 m4 k4. More... | |
class | pyNastran.bdf.cards.aero.PAERO1 |
Defines associated bodies for the panels in the Doublet-Lattice method. More... | |
class | pyNastran.bdf.cards.aero.PAERO2 |
Defines the cross-sectional properties of aerodynamic bodies PAERO2 PID ORIENT WIDTH AR LRSB LRIB LTH1 LTH2 THI1 THN1 THI2 THN2 THI3 THN3. More... | |
class | pyNastran.bdf.cards.aero.Spline |
class | pyNastran.bdf.cards.aero.SPLINE1 |
Surface Spline Methods Defines a surface spline for interpolating motion and/or forces for aeroelastic problems on aerodynamic geometries defined by regular arrays of aerodynamic points. More... | |
class | pyNastran.bdf.cards.aero.SPLINE2 |
Linear Spline Defines a surface spline for interpolating motion and/or forces for aeroelastic problems on aerodynamic geometries defined by regular arrays of aerodynamic points. More... | |
class | pyNastran.bdf.cards.aero.SPLINE4 |
Surface Spline Methods Defines a curved surface spline for interpolating motion and/or forces for aeroelastic problems on general aerodynamic geometries using either the Infinite Plate, Thin Plate or Finite Plate splining method. More... | |
class | pyNastran.bdf.cards.aero.SPLINE5 |
Linear Spline Defines a 1D beam spline for interpolating motion and/or forces for aeroelastic problems on aerodynamic geometries defined by irregular arrays of aerodynamic points. More... | |
class | pyNastran.bdf.cards.aero.TRIM |
Packages | |
namespace | pyNastran::bdf::cards::aero |
Functions | |
def | pyNastran::bdf::cards::aero.__init__ |
def | pyNastran::bdf::cards::aero.rawFields |
Variables | |
string | pyNastran::bdf::cards::aero.type = 'AESURFS' |
pyNastran::bdf::cards::aero::id | |
pyNastran::bdf::cards::aero.label | |
pyNastran::bdf::cards::aero.list1 | |
pyNastran::bdf::cards::aero.list2 |