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.
Specifications
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