SUAVE.Analyses.Weights.Weights_eVTOL.Weights_eVTOL Class Reference

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

Public Member Functions
def	__defaults__ (self)
Public Member Functions inherited from SUAVE.Analyses.Weights.Weights.Weights
def	evaluate (self, conditions=None)
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 an eVTOL aircraft

Assumptions:
None

Source:
N/A

Inputs:
N/A

Outputs:
N/A

Properties Used:
N/A

Member Function Documentation

__defaults__()

def SUAVE.Analyses.Weights.Weights_eVTOL.Weights_eVTOL.__defaults__

(

self

)

Sets the default parameters for an eVTOL weight analysis

Assumptions:
None

Source:
N/A

Inputs:
N/A

Outputs:
N/A

Properties Used:
N/A

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

---

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

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