Auto Credit Based on david0327's Air Taxi design
This a conceptual design. During steady flight L/D = 0.089, zero lift drag = 0.29132. Lift coefficient at 10,000 feet = 0.5. Minimum power required =12325053.33 Newton. Equivalent loiter time = 43 minutes. Stall speed at 10,000 feet =Climb 27.84 m/s, max CL = 1.5. Climb angle = 38.7 Deg, Vertical speed = 38.8 m/s.
Specifications
General Characteristics
- Predecessor Air Taxi design
- Created On Windows
- Wingspan 43.8ft (13.4m)
- Length 47.0ft (14.3m)
- Height 17.0ft (5.2m)
- Empty Weight 5,104lbs (2,315kg)
- Loaded Weight 13,280lbs (6,024kg)
Performance
- Power/Weight Ratio 33.969
- Horse Power/Weight Ratio 0.301
- Wing Loading 38.8lbs/ft2 (189.5kg/m2)
- Wing Area 342.2ft2 (31.8m2)
- Drag Points 3787
Parts
- Number of Parts 280
- Control Surfaces 7
- Performance Cost 1,906
Hi folks, good to be back, this is the conceptual design for my school project. During gliding flight, the L/D = 1.25, sink rate = -18 m/s. Required landing distance under traditional landing Technic = 1603.8 meters.