SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976 Class Reference
Inheritance diagram for SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976:
SUAVE.Analyses.Atmospheric.Atmospheric.Atmospheric SUAVE.Analyses.Analysis.Analysis

Public Member Functions

def __defaults__ (self)
 
def compute_values (self, altitude, temperature_deviation=0.0, var_gamma=False)
 
- 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 the U.S. Standard Atmosphere (1976 version)
    
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.US_Standard_1976.US_Standard_1976.__defaults__ (   self)
This sets the default values for the analysis to function.

Assumptions:
None

Source:
N/A

Inputs:
None

Output:
None

Properties Used:
None

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

◆ compute_values()

def SUAVE.Analyses.Atmospheric.US_Standard_1976.US_Standard_1976.compute_values (   self,
  altitude,
  temperature_deviation = 0.0,
  var_gamma = False 
)
Computes atmospheric values.

Assumptions:
US 1976 Standard Atmosphere

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

Inputs:
altitude                                 [m]
temperature_deviation                    [K]

Output:
atmo_data.
  pressure                               [Pa]
  temperature                            [K]
  speed_of_sound                         [m/s]
  dynamic_viscosity                      [kg/(m*s)]
  kinematic_viscosity                    [m^2/s]
  thermal_conductivity                   [W/(m*K)]
  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]
    temperature                          [K]
    pressure                             [Pa]

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