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_start | |
altitude_end | |
descent_rate | |
mach_end | |
mach_start | |
true_course | |
Public Attributes inherited from SUAVE.Analyses.Mission.Segments.Climb.Unknown_Throttle.Unknown_Throttle | |
altitude_start | |
altitude_end | |
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 | |
Change Mach numbers during a descent while descending at a constant rate. The Mach number changes linearly throughout the descent. Assumptions: None Source: None
def SUAVE.Analyses.Mission.Segments.Descent.Linear_Mach_Constant_Rate.Linear_Mach_Constant_Rate.__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.Climb.Unknown_Throttle.Unknown_Throttle.