pyNastran  0.5.0
pyNastran BDF Reader/Writer, OP2 Parser, and GUI
aero.py File Reference

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
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