I want to define a OEI (one engine inoperative) configuration that has added drag due to thrust asymetry.
I want to use "aerodynamics.settings.spoiler_drag_increment = 0.xx" setting for that.
I found no way to do this with inside the configuration builder:
config = SUAVE.Components.Configs.Config(base_config)
config.tag = 'oei'
### I want to add spoiler drag here ####
configs.append(config)
What I can do, is adjust the spoiler drag later, when I define the mission:
# ------------------------------------------------------------------
# Cruise Segment: Constant Mach, Constant Altitude
# ------------------------------------------------------------------
segment = Segments.Cruise.Constant_Mach_Constant_Altitude(base_segment)
segment.tag = "oei_cruise"
segment.analyses.extend( analyses.oei)
analyses.oei.aerodynamics.settings.spoiler_drag_increment = 0.1 #set drag-points here --> will be ADDED to cd0
segment.altitude = 35000 * Units.ft
segment.mach = 0.7
segment.distance = 10 * Units.km
I just don't like it, since I have to keep track of these setting for each mission segment.
My question:
How can I define spoiler drag for each configuration?
Thank you
Matthias