SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid Class Reference

Inheritance diagram for SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid:

Public Member Functions
def	__defaults__ (self)
def	initialize (self)
def	evaluate (self, state, settings, geometry)
def	sample_training (self)
def	build_surrogate (self)
Public Member Functions inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
def	evaluate (self, state)
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
	geometry
	settings
	training
	training_file
	surrogates
Public Attributes inherited from SUAVE.Analyses.Aerodynamics.Aerodynamics.Aerodynamics
	tag
	geometry
	settings
Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis
	tag
	features
	settings

Detailed Description

This builds a surrogate and computes lift and drag using SU2

Assumptions:
Inviscid, subsonic

Source:
None

Member Function Documentation

__defaults__()

def SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid.__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.Aerodynamics.Aerodynamics.Aerodynamics.

build_surrogate()

def SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid.build_surrogate

(

self

)

Builds a surrogate based on sample evalations using a Guassian process.

Assumptions:
None

Source:
N/A

Inputs:
self.training.
  coefficients     [-] CL and CD
  grid_points      [radians,-] angles of attack and mach numbers 

Outputs:
self.surrogates.
  lift_coefficient <Guassian process surrogate>
  drag_coefficient <Guassian process surrogate>

Properties Used:
No others

evaluate()

def SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid.evaluate	(		self,
			state,
			settings,
			geometry
	)

Evaluates lift and drag using available surrogates.

Assumptions:
None

Source:
N/A

Inputs:
state.conditions.
  mach_number      [-]
  angle_of_attack  [radians]

Outputs:
inviscid_lift      [-] CL
inviscid_drag      [-] CD

Properties Used:
self.surrogates.
  lift_coefficient [-] CL
  drag_coefficient [-] CD

initialize()

def SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid.initialize

(

self

)

Drives functions to get training samples and build a surrogate.

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
None

sample_training()

def SUAVE.Analyses.Aerodynamics.SU2_inviscid.SU2_inviscid.sample_training

(

self

)

Call methods to run SU2 for sample point evaluation.

Assumptions:
None

Source:
N/A

Inputs:
see properties used

Outputs:
self.training.
  coefficients     [-] CL and CD
  grid_points      [radians,-] angles of attack and mach numbers 

Properties Used:
self.geometry.tag  <string>
self.training.     
  angle_of_attack  [radians]
  Mach             [-]
self.training_file (optional - file containing previous AVL data)

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

• /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Analyses/Aerodynamics/SU2_inviscid.py