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

Public Member Functions

def __defaults__ (self)
 
def finalize (self)
 
def __call__ (self, conditions)
 
- Public Member Functions inherited from SUAVE.Analyses.Stability.Stability.Stability
def evaluate (self, conditions)
 
- 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

 configuration
 
 geometry
 
- Public Attributes inherited from SUAVE.Analyses.Stability.Stability.Stability
 tag
 
 geometry
 
 settings
 
- Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
 tag
 
 features
 
 settings
 

Detailed Description

This is an analysis based on low-fidelity models.

Assumptions:
Subsonic

Source:
Primarily based on adg.stanford.edu, see methods for details

Member Function Documentation

◆ __call__()

def SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.__call__ (   self,
  conditions 
)
Process vehicle to setup geometry, condititon and configuration

Assumptions:
None

Source:
N/4

Inputs:
conditions - DataDict() of aerodynamic conditions
results    - DataDict() of moment coeffients and stability and body axis derivatives

Outputs:
None

Properties Used:
self.geometry

◆ __defaults__()

def SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.__defaults__ (   self)
This sets the default values and methods for the analysis.

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

Reimplemented from SUAVE.Analyses.Stability.Stability.Stability.

◆ finalize()

def SUAVE.Analyses.Stability.Fidelity_Zero.Fidelity_Zero.finalize (   self)
Finalizes the surrogate needed for lift calculation.

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
self.geometry

Reimplemented from SUAVE.Analyses.Stability.Stability.Stability.


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