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 | |
This is class that evaluates the weight of Transport class aircraft Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: N/A
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.
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.