Definition Parameters
| Dimension |
Value (inlbs) |
Value (mkgs) |
| Wingspan |
72 in |
1.8288 m |
| Wing Break |
15.20 in |
0.38608 m |
| Root Chord |
20.57 in |
0.5224 m |
| Mid Chord |
13.668 in |
0.3471 m |
| Tip Chord |
8.23 in |
0.2091 m |
| LE Sweep |
4.84 degrees |
4.84 degrees |
| MTOW |
14.4 lbs |
6.532 kg |
| Load Factor |
10 |
10 |
| Spar Width |
1.9685 in |
0.05 m |
| Spar Location |
24.9% chord |
24.9% chord |
| Airfoil |
SD5060 |
SD5060 |
| LE loc from dtm |
20 in |
0.508 m |
| AOI |
2 degrees |
2 degrees |
| Global Z Offset |
2 in |
0.0508 m |
Deviations from Definition
- Root and tip foil scaled by 5%, 10% to create ~1/16in finite TE
- Root spar location WAS: 24.9% (5.122 in) IS: 30.1% (6.377 in)
- Tip spar angled to end at 24.9% chord, meet M1 section spar
Wing Definition
Stations/Sections
| Station |
y (in) |
| Root |
0 |
| Mid |
15.2 |
| Tip |
36 |
Spar Area Dimensions
| Station |
Avg. Height (in) |
Width (in) |
| Root |
2.0233 |
1.9685 |
| Mid |
1.518 |
1.9685 |
| Tip |
0.81366 |
1.9685 |
| Section |
y range (in) |
| Root |
0 → 15.2 |
| Tip |
15.2 → 36 |
Spar Code Input (ALL CODE INPUT AND OUTPUT IN SI)
Spar Code Output (ALL CODE INPUT AND OUTPUT IN SI)
- Spar Cap Width $w=50mm$
- Shear Web Layup: 1x 2.74oz Fiberglass
- One Sparcap Mass Estimate: 0.05971 kg → 0.132 lbs
- For entire wing (x4): 0.2388 kg → 0.527 lbs
Spar Cap Layup (one cap)
| y range (m) |
y range (in) |
Layup |
| S1: 0 → 0.2798 |
0 → 11.016 |
$[U / U]$ |
| S2: 0.2798 → 0.9144 |
11.016 → 36 |
$[U]$ |