Public Member Functions | |
def | __defaults__ (self) |
Public Member Functions inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment | |
def | initialize (self) |
def | converge (self, state) |
def | iterate (self) |
def | finalize (self) |
def | evaluate (self, state=None) |
def | merged (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 | |
altitude | |
mach | |
distance | |
true_course | |
Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude | |
altitude | |
air_speed | |
distance | |
true_course | |
Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Aerodynamic.Aerodynamic | |
temperature_deviation | |
Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Segment.Segment | |
settings | |
state | |
analyses | |
process | |
conditions | |
Public Attributes inherited from SUAVE.Analyses.Analysis.Analysis | |
tag | |
features | |
settings | |
Vehicle flies at a constant Mach number at a set altitude for a fixed distance Assumptions: Built off of a constant speed constant altitude segment Source: None
def SUAVE.Analyses.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude.Constant_Mach_Constant_Altitude.__defaults__ | ( | self | ) |
This sets the default solver flow. Anything in here can be modified after initializing a segment. Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: None
Reimplemented from SUAVE.Analyses.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude.Constant_Speed_Constant_Altitude.