SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics Class Reference

Inheritance diagram for SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics:

Public Member Functions
def	__defaults__ (self)
Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Conditions.Conditions.Conditions
def	ones_row (self, cols)
def	ones_row_m1 (self, cols)
def	ones_row_m2 (self, cols)
def	expand_rows (self, rows, override=False)

Public Attributes
	tag
	freestream
	aerodynamics
	stability
	aero_derivatives
	propulsion
	noise
Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic
	tag
	frames
	weights
	energies
	noise

Detailed Description

This builds upon Basic, which itself builds on conditions, to add the data structure for aerodynamic mission analyses.

    Assumptions:
    None
    
    Source:
    None

Member Function Documentation

__defaults__()

def SUAVE.Analyses.Mission.Segments.Conditions.Aerodynamics.Aerodynamics.__defaults__

(

self

)

This sets the default values.
    
    Assumptions:
    None
    
    Source:
    N/A
    
    Inputs:
    None
    
    Outputs:
    None
    
    Properties Used:
    None

Reimplemented from SUAVE.Analyses.Mission.Segments.Conditions.Basic.Basic.

Reimplemented in SUAVE.Analyses.Aerodynamics.AVL_Inviscid.AVL_Inviscid.

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

• /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Mission/Segments/Conditions/Aerodynamics.py