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XF-58 Dominator (Revised)

818 JoffahSanno  9.7 years ago
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Auto Credit Based on JoffahSanno's XF-58 Dominator

I edited the yaw to make it more responsive. I also reduced the size of the ailerons, adding more stability when rolling. Give me your criticism and comments and ill be happy to make changes to the design. Feel free to change whatever you'd like, but remember to rate what you think this plane deserves. :D

General Characteristics

  • Predecessor XF-58 Dominator
  • Created On iOS
  • Wingspan 26.0ft (7.9m)
  • Length 38.4ft (11.7m)
  • Height 7.3ft (2.2m)
  • Empty Weight 11,056lbs (5,015kg)
  • Loaded Weight 14,524lbs (6,588kg)

Performance

  • Power/Weight Ratio 2.32
  • Wing Loading 45.8lbs/ft2 (223.6kg/m2)
  • Wing Area 317.2ft2 (29.5m2)
  • Drag Points 1878

Parts

  • Number of Parts 75
  • Control Surfaces 11
  • Performance Cost 313
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    @thomasjaf oh ok I see now, thanks for the tip, I didnt realize it worked like that haha
    9.7 years ago
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    6,104 thomasjaf
    For pitch control surface, if it's behind the COM then it should "push down" to pitch up ( the surface goes upward), if it's in front of the COM the surface should lift the noze (the surface goes downwards). Try to remove the pitching surface at the rear to understand better. And was it clear?
    9.7 years ago
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    @thomasjaf yes, I did not see much of a difference if they are inverted or not, but I am a new user and still learning the basics. Could you explain why I should invert them please? Thank you you!
    9.7 years ago
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    6,104 thomasjaf
    Are your canard ailerons not inverted on purpose?
    9.7 years ago