carboLAB
Experimental 2010 design: two rows...
Flat area = 26.06 m2
Flat span = 14.00 m
Flat A/R = 7.52
LE.txt (airfoil)
leparagliding.txt (file code)
le-3D.dwg download 3d dwg model
(Internal V-rib design under study...)
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* LABORATORI
D'ENVOL PARAGLIDING
DESIGN
*
* Input data
file
*
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*
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*
1.
GEOMETRY
*
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* Wing name
carboLAB
* Number of cells
83
* Number of ribs
84
* Alpha max
5.2
* Rib geometric parameters
*
Rib x-rib y-LE
y-TE xp z
beta RP
1
0.05 0.00 230.84
0.05 0.00 0.00
33.33
2
18.14 0.00 230.81
18.14 0.05 1.23
33.33
3
34.70 0.17 230.74
34.69 0.77 2.48
33.33
4
51.27 0.37 230.62
51.24 1.48 4.00
33.33
5
67.83 0.65 230.45
67.77 2.51 4.60
33.33
6
84.40 1.00 230.23
84.27 3.91 6.00
33.33
7
100.96 1.44
229.97 100.72
5.89 6.89 33.33
8
117.52 1.95
229.66 117.16
7.88 9.41 33.33
9
134.09 2.54
229.30 133.49
10.65 10.20 33.33
10
150.65 3.21
229.30 149.74
13.86 11.17 33.33
11
167.21 3.96
228.90 165.99
17.06 14.37 33.33
12
183.78 4.80
228.44 182.23
20.32 15.50 33.33
13
200.34 5.71
227.93 198.27
24.46 16.30 33.33
14
218.09 6.78
227.37 214.10
29.34 17.22 33.33
15
235.83 7.95
226.71 231.06
34.56 19.00 33.33
16
253.58 9.22
225.99 247.95
40.00 20.45 33.33
17
271.33 10.59
225.21 264.58
46.20 22.00 33.33
18
289.07 12.06
224.37 281.05
52.82 23.33 33.33
19
306.82 13.63
223.46 297.34
59.85 25.00 33.33
20
324.57 15.31
222.48 313.51
67.20 26.46 33.33
21
342.31 17.10
221.43 329.39
75.10 28.80 33.33
22
360.06 18.99
220.31 345.14
83.31 30.00 33.33
23
377.81 21.01
219.12 360.50
92.18 31.04 33.33
24
395.55 23.14
217.84 375.87
101.05 32.00 33.33
25
413.30 25.39
216.49 390.95
110.42 33.05 33.33
26
431.05 27.76
215.05 405.76
120.20 35.00 33.33
27
448.79 30.27
213.52 420.26
130.43 37.50 33.33
28
466.54 32.91
211.89 434.49
141.35 38.61 33.33
29
484.29 35.69
210.16 447.71
153.19 42.64 33.33
30
502.03 39.11
208.32 460.58
165.40 46.76 33.33
31
519.78 43.01
206.37 472.38
178.66 51.08 33.33
32
537.53 47.42
204.29 483.53
192.47 52.60 33.33
33
555.27 52.33
202.08 493.85
206.90 56.51 33.33
34
573.02 57.77
199.72 503.54
221.78 60.40 33.33
35
590.77 63.74
197.19 512.04
237.35 63.86 33.33
36
608.51 70.25
194.47 519.74
253.07 67.06 33.33
37
626.26 77.34
191.55 526.54
269.73 69.11 33.33
38
643.22 85.48
188.38 532.22
286.27 72.94 33.33
39
657.72 94.10
185.09 536.87
302.58 75.97 33.33
40
673.38 105.45
182.03 539.98
316.35 76.73 33.33
41
686.43 116.87
178.42 543.44
327.83 71.90 33.33
42
700.00 131.17
175.11 551.09
339.01 48.70 33.33
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*
2. AIRFOILS
*
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* Airfoil name. intake in. intake out. open
1 LE.txt 1.2 5.5 1
2 LE.txt 1.2 5.5 1
3 LE.txt 1.2 5.5 1
4 LE.txt 1.2 5.5 1
5 LE.txt 1.2 5.5 1
6 LE.txt 1.2 5.5 1
7 LE.txt 1.2 5.5 1
8 LE.txt 1.2 5.5 1
9 LE.txt 1.2 5.5 1
10 LE.txt 1.2 5.5 1
11 LE.txt 1.2 5.5 1
12 LE.txt 1.2 5.5 1
13 LE.txt 1.2 5.5 1
14 LE.txt 1.2 5.5 1
15 LE.txt 1.2 5.5 1
16 LE.txt 1.2 5.5 1
17 LE.txt 1.2 5.5 1
18 LE.txt 1.2 5.5 1
19 LE.txt 1.2 5.5 1
20 LE.txt 1.2 5.5 1
21 LE.txt 1.2 5.5 1
22 LE.txt 1.2 5.5 1
23 LE.txt 1.2 5.5 1
24 LE.txt 1.2 5.5 1
25 LE.txt 1.2 5.5 1
26 LE.txt 1.2 5.5 1
27 LE.txt 1.2 5.5 1
28 LE.txt 1.2 5.5 1
29 LE.txt 1.2 5.5 1
30 LE.txt 1.2 5.5 1
31 LE.txt 1.2 5.5 1
32 LE.txt 1.2 5.5 1
33 LE.txt 1.2 5.5 1
34 LE.txt 1.2 5.5 1
35 LE.txt 1.2 5.5 1
36 LE.txt 1.2 5.5 0
37 LE.txt 1.2 5.5 0
38 LE.txt 1.2 5.5 0
39 LE.txt 1.2 5.5 0
40 LE.txt 1.2 5.5 0
41 LE.txt 1.2 5.5 0
42 LE.txt 1.2 5.5 0
*************************************************************
*
3. ANCHOR
POINTS
*
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*
Airf Anch A
B C D
E F
1
0 0 0
0 0 0 0
2
0 0 0
0 0 0 0
3
3 15.5 23.6
67.5 0 0 100
4
0 0 0
0 0 0 0
5
0 0 0
0 0 0 0
6
3 15.5 23.6
67.5 0 0 100
7
0 0 0
0 0 0 0
8
0 0 0
0 0 0 0
9
3 15.5 23.6
67.5 0 0 100
10
0 0 0
0 0 0 0
11
0 0 0
0 0 0 0
12
3 15.5 23.6
67.5 0 0 100
13
0 0 0
0 0 0 0
14
0 0 0
0 0 0 0
15
0 0 0
0 0 0 100
16
0 0 0
0 0 0 0
17
3 15.5 23.6
67.5 0 0 0
18
0 0 0
0 0 0 100
19
0 0 0
0 0 0 0
20
3 15.5 23.6
67.5 0 0 0
21
0 0 0
0 0 0 100
22
0 0 0
0 0 0 0
23
3 15.5 23.6
67.5 0 0 0
24
0 0 0
0 0 0 100
25
0 0 0
0 0 0 0
26
3 15.5 23.6
67.5 0 0 0
27
0 0 0
0 0 0 100
28
0 0 0
0 0 0 0
29
0 0 0
0 0 0 0
30
0 0 0
0 0 0 0
31
2 16.22 70
0 0 0 100
32
2 16.22 70
0 0 0 0
33
0 0 0
0 0 0 0
34
2 16.22 70
0 0 0 100
35
2 16.22 70
0 0 0 0
36
0 0 0
0 0 0 0
37
2 16.22 70
0 0 0 100
38
2 16.22 70
0 0 0 0
39
0 0 0
0 0 0 0
40
2 15 70
0 0 0 100
41
2 8.0 70
0 0 0 0
42
0 0 0
0 0 0 0
*************************************************************
*
4. AIRFOIL
HOLES
*
*************************************************************
1
1
42
9
14.59 1.92 2.735 6.72 0.
22.18 1.78 2.375 6.72 0.
33.36 1.64 2.5 5.9 0.
40.32 1.46 2.4 5.8 0.
47.41 1.34 2.23 5.7 0.
59.17 1.27 1.84 3.4 0.
65.23 1.33 1.7 3.2 0.
71.21 1.18 1.6 3.0 0.
81.87 0.89 1.6 1.6 0.
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*
5. SKIN
TENSION
*
*************************************************************
Extrados
0. 0. 0. 0.
7.5 1.3 10. 1.33
15. 2.5 20. 2.5
80. 2.5 80. 2.5
90. 1.33 90. 1.33
100. 0.0 100. 0.
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*
6. SEWING
ALLOWANCES
*
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15 upper panels (mm)
15 lower panels (mm)
15 ribs (mm)
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* 7. MARKS
*************************************************************
50. 0.5
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*
8. Global angle of attack
estimation *
*************************************************************
* Finesse GR
10
* Center of pressure % of chord
50
* Calage %
42
* Risers lenght cm
55
* Line lenght cm
937
* Karabiners cm
40
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* 9. SUSPENSION LINES DESCRIPTION
***************************************************
3
14
4 1 1 2 1 3 1 4 1 1 3
4 1 1 2 1 3 1 4 2 1 6
4 1 1 2 1 3 2 4 3 1 9
4 1 1 2 1 3 2 4 4 1 12
4 1 1 2 2 3 3 4 5 1 17
4 1 1 2 2 3 3 4 6 1 20
4 1 1 2 2 3 4 4 7 1 23
4 1 1 2 2 3 4 4 8 1 26
4 1 1 2 3 3 5 4 9 1 31
4 1 1 2 3 3 5 4 10 1 32
4 1 1 2 3 3 6 4 11 1 34
4 1 1 2 3 3 6 4 12 1 35
4 1 1 2 3 3 7 4 13 1 37
4 1 1 2 3 3 7 4 14 1 38
4
4
1 1 2 1 3
1 4 1 1 40
4
1 1 2 1 3
1 4 2 2 40
4
1 1 2 1 3
1 4 3 1 41
4
1 1 2 1 3
1 4 4 2 41
14
4 1 1 2 1 3 1 4 1 3 3
4 1 1 2 1 3 1 4 2 3 6
4 1 1 2 1 3 2 4 3 3 9
4 1 1 2 1 3 2 4 4 3 12
4 1 1 2 2 3 3 4 5 3 17
4 1 1 2 2 3 3 4 6 3 20
4 1 1 2 2 3 4 4 7 3 23
4 1 1 2 2 3 4 4 8 3 26
4 1 1 2 3 3 5 4 9 2 31
4 1 1 2 3 3 5 4 10 2 32
4 1 1 2 3 3 6 4 11 2 34
4 1 1 2 3 3 6 4 12 2 35
4 1 1 2 3 3 7 4 13 2 37
4 1 1 2 3 3 7 4 14 2 38
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* 10. BRAKES
***************************************************
330
12
4 1 1 2 1 3 1 4 1 6 6
4 1 1 2 1 3 1 4 2 6 9
4 1 1 2 1 3 2 4 3 6 12
4 1 1 2 1 3 2 4 4 6 15
4 1 1 2 2 3 3 4 5 6 18
4 1 1 2 2 3 3 4 6 6 21
4 1 1 2 2 3 4 4 7 6 24
4
1 1 2 2 3 4 4
8 6 27
4 1 1 2 3 3 5 4 9 6 31
4 1 1 2 3 3 5 4 10 6 34
4 1 1 2 3 3 6 4 11 6 37
4 1 1 2 3 3 6 4 12 6 40
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* 11. Ramification lengths
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3 180
4 350 180
3 100
4 200 80
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