class Markup(Aerodynamics):
""" SUAVE.Analyses.Aerodynamics.Markup()
"""
def __defaults__(self):
self.tag = 'aerodynamics_markup'
self.geometry = Data()
self.settings = Data()
self.process = Process()
self.process.initialize = Process()
self.process.compute = Process()
def evaluate(self, state):
settings = self.settings
geometry = self.geometry
results = self.process.compute(state, settings, geometry)
return results
def initialize(self):
self.process.initialize(self)
class Markup(Aerodynamics):
""" SUAVE.Analyses.Aerodynamics.Markup()
"""
def __defaults__(self):
self.tag = 'aerodynamics_markup'
self.geometry = Data()
self.settings = Data()
self.process = Process()
self.process.initialize = Process()
self.process.compute = Process()
def evaluate(self,state):
settings = self.settings
geometry = self.geometry
results = self.process.compute(state,settings,geometry)
return results
def initialize(self):
self.process.initialize(self)
class Markup(Aerodynamics):
"""This is an intermediate class for aerodynamic analyses.
Assumptions:
None
Source:
N/A
"""
def __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
"""
self.tag = 'aerodynamics_markup'
self.geometry = Data()
self.settings = Data()
self.process = Process()
self.process.initialize = Process()
self.process.compute = Process()
def evaluate(self,state):
"""The default evaluate function.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
results <SUAVE data class>
Properties Used:
self.settings
self.geometry
"""
settings = self.settings
geometry = self.geometry
results = self.process.compute(state,settings,geometry)
return results
def initialize(self):
"""The default finalize function. Calls the initialize process.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A
"""
self.process.initialize(self)
class Markup(Aerodynamics):
"""This is an intermediate class for aerodynamic analyses.
Assumptions:
None
Source:
N/A
"""
def __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
"""
self.tag = 'aerodynamics_markup'
self.geometry = Data()
self.settings.lift_to_drag_adjustment = 0. # (.1 is a 10% increase in L/D over base analysis)
# this is applied directly to the final drag value
self.process = Process()
self.process.initialize = Process()
self.process.compute = Process()
def evaluate(self,state):
"""The default evaluate function.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
results <SUAVE data class>
Properties Used:
self.settings
self.geometry
"""
settings = self.settings
geometry = self.geometry
results = self.process.compute(state,settings,geometry)
return results
def initialize(self):
"""The default finalize function. Calls the initialize process.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A
"""
self.process.initialize(self)
class Markup(Aerodynamics):
"""This is an intermediate class for aerodynamic analyses.
Assumptions:
None
Source:
N/A
"""
def __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
"""
self.tag = 'aerodynamics_markup'
self.geometry = Data()
self.settings = Data()
self.process = Process()
self.process.initialize = Process()
self.process.compute = Process()
def evaluate(self, state):
"""The default evaluate function.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
results <SUAVE data class>
Properties Used:
self.settings
self.geometry
"""
settings = self.settings
geometry = self.geometry
results = self.process.compute(state, settings, geometry)
return results
def initialize(self):
"""The default finalize function. Calls the initialize process.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A
"""
self.process.initialize(self)
class Markup(Aerodynamics):
"""This is an intermediate class for aerodynamic analyses.
Assumptions:
None
Source:
N/A
"""
def __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
"""
self.tag = 'aerodynamics_markup'
self.geometry = Data()
self.settings.maximum_lift_coefficient_factor = 1.0
self.settings.lift_to_drag_adjustment = 0. # (.1 is a 10% increase in L/D over base analysis)
# this is applied directly to the final drag value
self.process = Process()
self.process.initialize = Process()
self.process.compute = Process()
def evaluate(self, state):
"""The default evaluate function.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
results <SUAVE data class>
Properties Used:
self.settings
self.geometry
"""
settings = self.settings
geometry = self.geometry
results = self.process.compute(state, settings, geometry)
return results
def initialize(self):
"""The default finalize function. Calls the initialize process.
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A
"""
self.process.initialize(self)
