SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics Class Reference

Inheritance diagram for SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics:

Public Member Functions
def	__defaults__ (self)
def	evaluate (self, state)
def	finalize (self)
Public Member Functions inherited from SUAVE.Analyses.Analysis.Analysis
def	compile (self, *args, **kwarg)
def	initialize (self, *args, **kwarg)
def	evaluate (self, *args, **kwarg)
def	finalize (self, *args, **kwarg)
def	__call__ (self, *args, **kwarg)

Public Attributes
	tag
	geometry
	settings
Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
	tag
	features
	settings

Detailed Description

This is the base class for aerodynamics analyses. It contains functions
that are built into the default class.

Assumptions:
None

Source:
N/A

Member Function Documentation

__defaults__()

def SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.__defaults__

(

self

)

This sets the default values and methods for the analysis.

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

Reimplemented from SUAVE.Analyses.Analysis.Analysis.

Reimplemented in SUAVE.Analyses.Aerodynamics.Vortex_Lattice.Vortex_Lattice, SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid, SUAVE.Analyses.Aerodynamics.SU2_Euler_Super.SU2_Euler_Super, SUAVE.Analyses.Aerodynamics.SU2_inviscid_Super.SU2_inviscid_Super, SUAVE.Analyses.Aerodynamics.SU2_Euler.SU2_Euler, SUAVE.Analyses.Aerodynamics.Fidelity_Zero.Fidelity_Zero, SUAVE.Analyses.Aerodynamics.Supersonic_OpenVSP_Wave_Drag.Supersonic_OpenVSP_Wave_Drag, SUAVE.Analyses.Aerodynamics.Supersonic_Zero.Supersonic_Zero, SUAVE.Analyses.Aerodynamics.AVL.AVL, SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS, SUAVE.Analyses.Aerodynamics.Lifting_Line.Lifting_Line, and SUAVE.Analyses.Aerodynamics.Markup.Markup.

evaluate()

def SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.evaluate	(		self,
			state
	)

The default evaluate function.

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
results   <Results class> (empty)

Properties Used:
N/A

Reimplemented in SUAVE.Analyses.Aerodynamics.Markup.Markup.

finalize()

def SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics.finalize

(

self

)

The default finalize function.

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

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The documentation for this class was generated from the following file:

• /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/Aerodynamics.py