SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS Class Reference

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

Public Member Functions
def	__defaults__ (self)
Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
def	evaluate (self, state)
def	initialize (self)
Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
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
Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Markup.Markup
	tag
	geometry
	process
Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
	tag
	geometry
	settings
Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
	tag
	features
	settings

Detailed Description

This is an analysis based on the AERODAS models.

Assumptions:
None

Source:
NASA TR: "Models of Lift and Drag Coefficients of Stalled and Unstalled Airfoils in
  Wind Turbines and Wind Tunnels" by D. A. Spera

Member Function Documentation

__defaults__()

def SUAVE.Analyses.Aerodynamics.AERODAS.AERODAS.__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.Aerodynamics.Markup.Markup.

---

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

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