************************************************************** * LABORATORI D'ENVOL PARAGLIDING DESIGN * * Input data file * ************************************************************** * Update 2017-6-18 ************************************************************** * 1. GEOMETRY * ************************************************************** * Brand name "Laboratori d'envol" * Wing name "gnuPSF" * Drawing scale 1.0 * Wing scale 1.0 * Number of cells 19 * Number of ribs 20 * Alpha wingtip, parameter, (alpha center) 10.0 0 0.0 * Paraglider type and parameter "ss" 1 * Rib geometric parameters * Rib x-rib y-LE y-TE xp z beta RP Washin 1 19.74 .00 250.00 19.73 .44 2.50 33.33 .00 2 59.21 .00 250.00 59.03 3.97 7.63 33.33 .00 3 98.68 .01 249.99 97.86 10.99 12.76 33.33 .00 4 138.16 .01 249.99 135.91 21.46 17.97 33.33 .00 5 177.63 .02 249.98 172.87 35.28 23.06 33.33 .00 6 217.11 .03 249.97 208.45 52.35 28.15 33.33 1.00 7 256.58 .04 249.96 242.36 72.53 33.37 33.33 2.50 8 296.05 .06 249.94 274.33 95.66 38.46 33.33 5.00 9 335.53 .07 249.93 304.11 121.55 43.55 33.33 7.50 10 375.00 .09 249.91 331.45 150.00 48.64 33.33 10.00 ************************************************************** * 2. AIRFOILS * ************************************************************** * Airfoil name. intake in. intake out. open. disp rweight 1 gnuPSF.txt 2.244 10.0 1 0 1 1 2 gnuPSF.txt 2.244 10.0 1 0 1 1 3 gnuPSF.txt 2.244 10.0 1 0 1 1 4 gnuPSF.txt 2.244 10.0 1 0 1 1 5 gnuPSF.txt 2.244 10.0 1 0 1 1 6 gnuPSF.txt 2.244 10.0 1 0 1 1 7 gnuPSF.txt 2.244 10.0 1 0 1 1 8 gnuPSF.txt 2.244 10.0 1 0 1 1 9 gnuPSF.txt 2.244 10.0 1 0 1 1 10 gnuPSF.txt 2.244 10.0 1 0 1 1 ************************************************************* * 3. ANCHOR POINTS * ************************************************************* * Airf Anch A B C D E F 1 4 10. 30.35 51.32 75.28 0 100 2 4 10. 30.35 51.32 75.28 0 100 3 4 10. 30.35 51.32 75.28 0 100 4 4 10. 30.35 51.32 75.28 0 100 5 4 10. 30.35 51.32 75.28 0 100 6 4 10. 30.35 51.32 75.28 0 100 7 4 10. 30.35 51.32 75.28 0 100 8 4 10. 30.35 51.32 75.28 0 100 9 4 10. 30.35 51.32 75.28 0 100 10 4 10. 30.35 51.32 75.28 0 100 ************************************************************* * 4. AIRFOIL HOLES * ************************************************************* 1 1 10 1 1 8.59 1.92 3. 3. 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. 0.0001 1000 1.0 ************************************************************* * 6. SEWING ALLOWANCES * ************************************************************* 15 25 25 upper panels (mm) 15 25 25 lower panels (mm) 15 ribs (mm) 15 vribs (mm) ************************************************************* * 7. MARKS ************************************************************* 25. 0.5 0.15 ************************************************************ * 8. Global angle of attack estimation * ************************************************************* * Finesse GR 4.5 * Center of pressure % of chord 35 * Calage % 27.8 * Risers lenght cm 47 * Line lenght cm 550 * Karabiners cm 40 *************************************************** * 9. SUSPENSION LINES DESCRIPTION *************************************************** 0 2 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 1 3 3 1 1 2 2 3 4 0 0 1 4 3 1 1 2 2 3 5 0 0 1 5 3 1 1 2 2 3 6 0 0 1 6 3 1 1 2 3 3 7 0 0 1 7 3 1 1 2 3 3 8 0 0 1 8 3 1 1 2 3 3 9 0 0 1 9 3 1 1 2 4 3 10 0 0 2 1 3 1 1 2 4 3 11 0 0 2 2 3 1 1 2 4 3 12 0 0 2 3 3 1 1 2 5 3 13 0 0 2 4 3 1 1 2 5 3 14 0 0 2 5 3 1 1 2 5 3 15 0 0 2 6 3 1 1 2 6 3 16 0 0 2 7 3 1 1 2 6 3 17 0 0 2 8 3 1 1 2 6 3 18 0 0 2 9 3 1 1 2 7 3 19 0 0 1 10 3 1 1 2 7 3 20 0 0 2 10 20 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 1 3 3 0 0 3 3 3 1 1 2 2 3 4 0 0 3 4 3 1 1 2 2 3 5 0 0 3 5 3 1 1 2 2 3 6 0 0 3 6 3 1 1 2 3 3 7 0 0 3 7 3 1 1 2 3 3 8 0 0 3 8 3 1 1 2 3 3 9 0 0 3 9 3 1 1 2 4 3 10 0 0 4 1 3 1 1 2 4 3 11 0 0 4 2 3 1 1 2 4 3 12 0 0 4 3 3 1 1 2 5 3 13 0 0 4 4 3 1 1 2 5 3 14 0 0 4 5 3 1 1 2 5 3 15 0 0 4 6 3 1 1 2 6 3 16 0 0 4 7 3 1 1 2 6 3 17 0 0 4 8 3 1 1 2 6 3 18 0 0 4 9 3 1 1 2 7 3 19 0 0 3 10 3 1 1 2 7 3 20 0 0 4 10 *************************************************** * 10. BRAKES *************************************************** 200 6 3 1 1 2 1 3 1 0 0 6 1 3 1 1 2 1 3 2 0 0 6 2.5 3 1 1 2 1 3 3 0 0 6 4 3 1 1 2 2 3 4 0 0 6 5 3 1 1 2 2 3 5 0 0 6 7 3 1 1 2 2 3 6 0 0 6 9 * Brake distribution 0 25 50 80 100 0 0 0 0 0 *************************************************** * 11. Ramification lengths *************************************************** 3 180 4 275 100 3 135 4 200 80 *************************************************** * 12. H V and VH ribs *************************************************** 1 80 150 1 5 2 1 1 1 50. 35. 85. 4.5 ***************************************************** * 15. Extrados colors ***************************************************** 3 1 1 1 40 0. 2 1 1 20 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