SUMMARY
OF WING GEOMETRY |
| PARAMETER NAME |
FIXED WING |
TILTWING |
| Aspect
Ratio (AR) |
3.56 |
5.76 |
| Sweep
(L) (deg) |
5 |
0 |
| Thickness-to-Chord
Ratio (t/c) (%) |
14 |
16 |
| Dihedral
(G) (deg) |
0 |
0 |
| Taper
Ratio (l) |
0.80 |
1.00 |
| Wing
Reference Area (Sref) (sq ft) |
1150 |
400 |
| Twist
Angle (e) (deg) |
-3 |
-2 |
| Incidence
Angle (iw) |
1 |
10 to 55 |
| Wing
Span (b) (ft) |
64 |
48 |
| Root
Chord (cr) (ft) |
19.97 |
8.33 |
| Tip
Chord (ct) (ft) |
15.97 |
8.33 |
| Mean
Aerodynamic Chord (mac) (ft) |
18.04 |
8.33 |
| Fuel
Volume (lb) |
17,505 |
10,854 |
SUMMARY OF
FIXED-WING TAIL GEOMETRY |
| PARAMETER NAME |
HORIZONTAL |
VERTICAL |
| Aspect
Ratio (AR) |
4.43 |
1.88 |
| Sweep
(L) (deg) |
5 |
5 |
| Thickness-to-Chord
Ratio (t/c) (%) |
12 |
10 |
| Dihedral
(G) (deg) |
0 |
N/A |
| Taper
Ratio (l) |
0.80 |
0.80 |
| Reference
Area (Sref) (sq ft) |
190 |
208 |
| Span
(b) (ft) |
29 |
14 |
| Root
Chord (cr) (ft) |
7.28 |
8.25 |
| Tip
Chord (ct) (ft) |
5.82 |
6.60 |
| Mean
Aerodynamic Chord (mac) (ft) |
6.58 |
7.46 |
| Volume
Coefficient |
0.21 |
0.06 |
SUMMARY OF
TILT-WING TAIL GEOMETRY |
| PARAMETER NAME |
HORIZONTAL |
VERTICAL |
| Aspect
Ratio (AR) |
3.46 |
2.61 |
| Sweep
(L) (deg) |
5 |
5 |
| Thickness-to-Chord
Ratio (t/c) (%) |
14 |
12 |
| Dihedral
(G) (deg) |
0 |
-- |
| Taper
Ratio (l) |
0.8 |
0.8 |
| Reference
Area (Sref) (sq ft) |
140 |
150 |
| Span
(b) (ft) |
24 |
14 |
| Root
Chord (cr) (ft) |
7.07 |
5.05 |
| Tip
Chord (ct) (ft) |
5.66 |
4.76 |
| Mean
Aerodynamic Chord (mac) (ft) |
6.39 |
5.38 |
| Volume
Coefficient |
1.21 |
0.24 |
SUMMARY OF FIXED-WING
CONTROL SURFACE GEOMETRY |
| CONTROL SURFACE |
PERCENT CHORD |
INBOARD
STATION(ft) |
OUTBOARD STATION(ft) |
| Rudder |
30 |
1.36 |
6.48 |
| Aileron |
30 |
24.54 |
31.42 |
| Elevator |
30 |
0.48 |
20.32 |
| Flaps |
30 |
7.43 |
23.11 |
| Slats |
30 |
entire
leading edge |
| Spoilers |
20 |
15.75 |
23.11 |
SUMMARY OF TILT-WING
CONTROL SURFACE GEOMETRY |
| CONTROL SURFACE |
PERCENT CHORD |
INBOARD
STATION(ft) |
OUTBOARD STATION(ft) |
| Rudder |
30 |
1.4 |
5.75 |
| Aileron |
30 |
16.8 |
23.76 |
| Elevator |
30 |
0.53 |
9.68 |
| Flaps |
30 |
7.43 |
14.75 |
| Slats |
30 |
entire
leading edge |
LINKS TO WING/EMPENNAGE DRAWINGS |
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