SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport Class Reference

Inheritance diagram for SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport:

Public Member Functions
def	__defaults__ (self)
def	evaluate (self, method="New SUAVE")
Public Member Functions inherited from SUAVE.Analyses.Weights.Weights.Weights
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
	vehicle
	settings
Public Attributes inherited from SUAVE.Analyses.Weights.Weights.Weights
	tag
	vehicle
	settings
	mass_properties
Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
	tag
	features
	settings

Detailed Description

This is class that evaluates the weight of Transport class aircraft

Assumptions:
    None

Source:
    N/A

Inputs:
    None

Outputs:
    None

Properties Used:
     N/A

Member Function Documentation

__defaults__()

def SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport.__defaults__

(

self

)

This sets the default values and methods for the tube and wing
aircraft weight analysis.

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

Reimplemented from SUAVE.Analyses.Weights.Weights.Weights.

evaluate()

def SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport.evaluate	(		self,
			method = "New SUAVE"
	)

Evaluate the weight analysis.

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
results

Properties Used:
N/A

Reimplemented from SUAVE.Analyses.Weights.Weights.Weights.

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

• /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Weights/Weights_Transport.py