SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport Class Reference
Inheritance diagram for SUAVE.Analyses.Weights.Weights_Transport.Weights_Transport:
SUAVE.Analyses.Weights.Weights.Weights SUAVE.Analyses.Analysis.Analysis

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.


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