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Canard flap experiment

48.8k Baldovino  6.5 years ago

A "simple" plane. Use TRIM for flaps and AOA of canards. Experiment using it in various % and with low engine rates to discover the aerodinamic changes. B for brakes.

General Characteristics

  • Created On Windows
  • Wingspan 34.1ft (10.4m)
  • Length 26.0ft (7.9m)
  • Height 8.4ft (2.6m)
  • Empty Weight 2,426lbs (1,100kg)
  • Loaded Weight 2,864lbs (1,299kg)

Performance

  • Horse Power/Weight Ratio 0.349
  • Wing Loading 10.8lbs/ft2 (52.6kg/m2)
  • Wing Area 265.7ft2 (24.7m2)
  • Drag Points 1301

Parts

  • Number of Parts 25
  • Control Surfaces 9
  • Performance Cost 276