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

Public Member Functions

def __defaults__ (self)
 
def compute_values (self, altitude, temperature=288.15)
 
- Public Member Functions inherited from SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric
def compute_values (self, altitude)
 
- 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)
 

Additional Inherited Members

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

Detailed Description

Implements a constant temperature with U.S. Standard Atmosphere (1976 version) freestream pressure
    
Assumptions:
None

Source:
U.S. Standard Atmosphere, 1976, U.S. Government Printing Office, Washington, D.C., 1976

Member Function Documentation

◆ __defaults__()

def SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature.__defaults__ (   self)
This sets the default values for the analysis to function.
    
Assumptions:
None
    
Source:
N/A
    
Inputs:
None
    
Outputs:
None
    
Properties Used:
None

Reimplemented from SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric.

◆ compute_values()

def SUAVE.Analyses.Atmospheric.Constant_Temperature.Constant_Temperature.compute_values (   self,
  altitude,
  temperature = 288.15 
)
Computes atmospheric values.
    
Assumptions:
Constant temperature atmosphere
    
Source:
U.S. Standard Atmosphere, 1976, U.S. Government Printing Office, Washington, D.C., 1976
    
Inputs:
altitude                                 [m]
temperature                              [K]

Outputs:
atmo_data.
  pressure                               [Pa]
  temperature                            [K]
  speed_of_sound                         [m/s]
  dynamic_viscosity                      [kg/(m*s)]
  prandtl_number                         [-]
    
Properties Used:
self.
  fluid_properties.gas_specific_constant [J/(kg*K)]
  planet.sea_level_gravity               [m/s^2]
  planet.mean_radius                     [m]
  breaks.
    altitude                             [m]
    pressure                             [Pa]

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