************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file version 2.52++ * ************************************************************** * ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "EF" * Wing name "PARAFOIL simple face" * Drawing scale 1.0 * Wing scale 0.185 * Number of cells 19 * Number of ribs 20 * Alpha max and parameter 4.5 0 * Paraglider type and parameter "ss" 1 * Rib geometric parameters * Rib x-rib y-LE y-TE xp z ANGLEPROFIL %CVR VRILLAGE 1 13.580 0 143.905 13.157 0.124 1.077 0 0.0 2 39.474 0 143.905 39.453 1.113 3.231 0 0.5 3 65.789 0 143.905 65.693 3.089 5.385 0 1.0 4 92.105 0 143.905 91.840 6.051 7.539 0 1.5 5 118.421 0 143.905 117.857 9.993 9.693 0 2.0 6 144.737 0 143.905 143.708 14.910 11.847 0 2.5 7 171.053 0 143.905 169.355 20.795 14.001 0 3.0 8 197.368 0 143.905 194.764 27.641 16.155 0 3.5 9 223.684 0 143.905 219.897 35.436 18.309 0 4.0 10 250.000 0 143.905 244.719 44.170 20.463 0 4.5 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name, intake in, intake out, open , disp. rrw 1 bhl2_01.txt 2.244 10.0 1 0 1 1 2 bhl2_01.txt 2.244 10.0 1 0 1 1 3 bhl2_01.txt 2.244 10.0 1 0 1 1 4 bhl2_01.txt 2.244 10.0 1 0 1 1 5 bhl2_01.txt 2.244 10.0 1 0 1 1 6 bhl2_01.txt 2.244 10.0 1 0 1 1 7 bhl2_01.txt 2.244 10.0 1 0 1 1 8 bhl2_01.txt 2.244 10.0 1 0 1 1 9 bhl2_01.txt 2.244 10.0 1 0 1 1 10 bhl2_01.txt 2.244 10.0 1 0 1 1 ************************************************************* * 3. ANCHOR POINTS * ************************************************************* * Airf Anch A B C D E F 1 4 10.00 30.35 51.32 75.28 0 0 2 4 10.00 30.35 51.32 75.28 0 0 3 4 10.00 30.35 51.32 75.28 0 0 4 4 10.00 30.35 51.32 75.28 0 0 5 4 10.00 30.35 51.32 75.28 0 0 6 4 10.00 30.35 51.32 75.28 0 0 7 4 10.00 30.35 51.32 75.28 0 0 8 4 10.00 30.35 51.32 75.28 0 0 9 4 10.00 30.35 51.32 75.28 0 0 10 4 10.00 30.35 51.32 75.28 0 0 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 1 1 14 1 1 0 0 0 0 0. 0. 0. ************************************************************* * 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. 0.0114 16 0.001 ************************************************************* * 6. SEWING ALLOWANCES * ************************************************************* 12 20 20 upper panels (mm) 12 20 20 lower panels (mm) 12 ribs (mm) 12 vribs (mm) ************************************************************* * 7. MARKS ************************************************************* 25. 0.5 0.15 ************************************************************ * 8. Global angle of attack estimation * ************************************************************* * Finesse GR 4.5 * Center of pressure % of chord 25 * Calage % 20 * Risers lenght cm 1 * Line lenght cm 655 * Karabiners cm 0.0001 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 0 3 20 3 1 1 2 1 3 1 0 0 1 1 3 1 1 2 1 3 2 0 0 1 2 3 1 1 2 1 3 3 0 0 2 1 3 1 1 2 1 3 4 0 0 2 2 3 1 1 2 2 3 5 0 0 1 3 3 1 1 2 2 3 6 0 0 1 4 3 1 1 2 2 3 7 0 0 2 3 3 1 1 2 2 3 8 0 0 2 4 3 1 1 2 3 3 9 0 0 1 5 3 1 1 2 3 3 10 0 0 1 6 3 1 1 2 3 3 11 0 0 2 5 3 1 1 2 3 3 12 0 0 2 6 3 1 1 2 4 3 13 0 0 1 7 3 1 1 2 4 3 14 0 0 1 8 3 1 1 2 4 3 15 0 0 2 7 3 1 1 2 4 3 16 0 0 2 8 3 1 1 2 5 3 17 0 0 1 9 3 1 1 2 5 3 18 0 0 1 10 3 1 1 2 5 3 19 0 0 2 9 3 1 1 2 5 3 20 0 0 2 10 10 3 1 1 2 1 3 1 0 0 3 1 3 1 1 2 1 3 2 0 0 3 2 3 1 1 2 2 3 3 0 0 3 3 3 1 1 2 2 3 4 0 0 3 4 3 1 1 2 3 3 5 0 0 3 5 3 1 1 2 3 3 6 0 0 3 6 3 1 1 2 4 3 7 0 0 3 7 3 1 1 2 4 3 8 0 0 3 8 3 1 1 2 5 3 9 0 0 3 9 3 1 1 2 5 3 10 0 0 3 10 10 3 1 1 2 1 3 1 0 0 4 1 3 1 1 2 1 3 2 0 0 4 2 3 1 1 2 2 3 3 0 0 4 3 3 1 1 2 2 3 4 0 0 4 4 3 1 1 2 3 3 5 0 0 4 5 3 1 1 2 3 3 6 0 0 4 6 3 1 1 2 4 3 7 0 0 4 7 3 1 1 2 4 3 8 0 0 4 8 3 1 1 2 5 3 9 0 0 4 9 3 1 1 2 5 3 10 0 0 4 10 *************************************************** * 10. BRAKES *************************************************** 100 1 3 1 1 2 1 3 1 0 0 6 1 * Brake distribution 0 25 55 70 100 0 0 0 0 0 *************************************************** * 11. Ramification lengths *************************************************** 3 110  4 150 100 3 100 4 200 70 *************************************************** * 12. H V and VH ribs *************************************************** 1 80 150 1 1 0 1 1 1 0.1 0 0 0 ***************************************************** * 15. Extrados colors ***************************************************** 3 1 1 1 40.1 0. 2 1 1 20.15 0. 3 1 1 0.0 0. ***************************************************** * 16. Intrados colors ***************************************************** 1 1 1 1 0. 0. ***************************************************** * 17. Aditional rib points ***************************************************** 2 8.288 7.27 11.21 -2.113 ***************************************************** * 18. Elastic lines corrections ***************************************************** 100 75 25 40 40 20 35 35 20 10 35 35 15 10 5 1 0.08 0.2 0.2 2 0.08 0.2 0.2 3 0.08 0.2 0.2 4 0.08 0.2 0.2 5 0.08 0.2 0.2