Inertia coupling is associated with longer fueselages with a concentration of weight at the extremities: the Natter wouldn't seem to qualify.
Something seems to have reduced the roll rate of the FW 190 when it was lengthened to accomodate the Jumo 213 V12 engine if Erick Browns recollections are to be accepted; certainly focke-wufl was trying to achieve something by fitting boosted airlerons if only maintain high speed roll.
One would think that the Do 335 might be vulnerable, however I suspect the aircrafts symetry, cruxiform empenage, counter rotating propellers and the gyroscopically stabalising effect of counter rotating propellers stabalised the aircraft or simply ensured that the principal axis on which it rolled aligned with the flight path axis well.
The pheomenum must have been present but not apparent in WW2.
Something seems to have reduced the roll rate of the FW 190 when it was lengthened to accomodate the Jumo 213 V12 engine if Erick Browns recollections are to be accepted; certainly focke-wufl was trying to achieve something by fitting boosted airlerons if only maintain high speed roll.
One would think that the Do 335 might be vulnerable, however I suspect the aircrafts symetry, cruxiform empenage, counter rotating propellers and the gyroscopically stabalising effect of counter rotating propellers stabalised the aircraft or simply ensured that the principal axis on which it rolled aligned with the flight path axis well.
The pheomenum must have been present but not apparent in WW2.
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