| SIZE |
AERODYNAMIC DATA |
| Total span – Kilometres |
3.015 |
|
Cruise |
Land & T/O |
| Wing chord – metres |
32.04 |
Wing Section |
NACA 64³-218 |
| Wing thickness – metres |
5.767 |
Flap chord |
25% |
| No of main floats |
101 |
Flap angle |
0° |
45° |
| Wing span between floats - m |
30.00 |
Angle of attack |
1.5° |
4.5° |
| |
|
Aspect ratio |
94.1 |
| Reflecting Strips |
|
Lift coefficient |
0.3 |
2.2 |
| Number |
400 |
Drag coefficient |
0.003 |
|
| Strip length - Kilometres |
8.333 |
Wing Reynolds no. |
1.2x108 |
4.5x107 |
| Length of fold – m |
7.2 |
V – m/sec |
55.7 |
20.6 |
| Width of fold – m |
7.0 |
V – ft/sec |
182.8 |
67.6 |
| Thickness of fold – mm |
4.0 |
V - knots |
108.3 |
40.0 |
| Number of folds |
1157 |
q – Kg/m² |
194.5 |
26.6 |
| Length of fold stowage tank – m |
4.63 |
|
|
|
| |
|
|
|
|
| WEIGHT |
HYDRODYNAMIC DATA |
| Estimates per spanwise metre |
|
Foil section based on |
NACA 64³-018 |
| Reflector system – Kg/m |
625 |
|
Main |
Rear |
| Engines + Fuel – Kg/m |
625 |
Float length - m |
16.0 |
9.36 |
| Structure + equipment – Kg/m |
625 |
Float Reynolds no. |
3.2x107 |
1.9x107 |
| Total weight – Kg/m |
1875 |
V - knots |
40.0 |
40.0 |
| Total craft weight – tonnes |
5625 |
q – Kg/m² |
2231.3 |
| Total engine power – Kw |
40000 |
|
|
|
| Number of engines |
51 |
|
|
|
