 LEPARAGLIDING PARTS. GUIDE OF INTERNAL CODE.

 0. HEADER (versions)

 1. VARIABLE NAMES

 2. VARIABLES TYPE DECLARATION

 3. INIT

 4. DATA READING

        4.1  Read main data file:

	     Read 1 Geometry (basic data and geometry)
	     Read 2 Airfoils
	     Read 3 Anchor points
	            Rib 0
	     Read 4 Holes
	     Read 5 Skin tension
	     Read 6 Sewing allowances
	     Read 7 Marks
	     Read 8 Calage estimation parameters
	     Read 9 Suspension lines desciption
                    Set default lines type (icase_lines=0)
	     Read 10 Brakes
                     Set default brakes type (icase_brakes=0)
	     Read 11 Ramification lengths
 	     Read 14 H V and HV ribs
	     Read 15 Extrados colors
             Read 16 Intrados colors
             Read 17 Additional rib points
             Read 18 Read elastic lines corrections
             Read 19 DXF layer names
             Read 20 marks types
             Read 21 joncs definition
             Read 22 nose mylars definition
             Read 23 tab reinforcements definition
             Read 24 general 2D DXF options
             Read 25 general 3D DXF options
             Read 26 general 3D DXF options
             Read 27 Special wingtip
             Read 28 Parameters for calage variation
             Read 29 3D-SHAPING
             Read 30 AIRFOIL THICKNESS MODIFICATION
             Read 31 New skin tension
             Read 32 parameters for part separation
             Read 33 Detailed risers
             Read 34 Lines characteristics table
             Read 35 Solve equilibrium equations
             Read 36 Create files for XFLR5 analysis
             Read 37 Read some special parameters

        4.2  Write xwimp geometry file for XFLR5
        4.3  Write some warnings and errors found in data
        4.3  Open some optional files (stl)
        4.4  Set some parameters (!)
	4.5 Center of gravity calculus (2D)
        4.6 Wing center of gravity calculus (3D)
        4.7 Adjust some parameters
             Rib(i,50)
             Rib and panel separation
             "pc" separation
             Lengths TE to A B C D E
        4.8 DXF layers (project)

 5. GRAPHIC DESIGN

	5.1 Planform drawing Box(1,1)
		5.1.1 Ribs
                5.1.2 Rotated ribs in "Z"
		5.1.3 LE
		5.1.4 TE
                5.1.5 Draw vents case k26d.eq.1
                      cases 0,1,4,5,6,-1,-2,-3,-4,-5,-6
                5.1.6 Draw vents case k26d.eq.0 "classic"
		5.1.7 Anchor points
                5.1.8 Brake points included fractionary points
                5.1.8+ Restitute virtual anchor for 3D if rib i+1 not defined
                5.1.9 Extrados colors (right)
                5.1.10 Intrados colors (left)
                5.1.11 Mini-ribs and middle ribs
		5.1.12 Draw special wintips

	5.2 Canopy drawing - vault Box(1,1)
               
	5.3 Boxes

 6. AIRFOILS coordinates calculus

        6.1 Read global points
	6.2 Read airfoil coordinates
	6.3 Airfoil coordinates*100
	6.4 Airfoil escaled and displaced coordinates
	6.5 Washin coordinates
	6.6 Space coordinates
	6.7 Absolute coordinates
	6.8 Treu desplaçament rib(i,50)
	6.9 Airfoil 0=1' assignation
	6.10 Assignation 3D coordinates airfoil 0
        6.10+ Compute TE-anchor lenghts along airfoil contour
	6.11 Compute external cutt edges in airfoils
        6.11+ Airfoils thickness
	6.12 Airfoils drawing

                Numering ribs (1,2) (2,2) (1,4)

                6.12.0 Miniribs - Minicabs (draw in airfoils)
                     Marks in 8.2.6

                6.12.1 Extrados
		Basic contour
		Basic contour washin
		Borders

                6.12.2 Inlets
                Case "pc"
                Case "ds" or "ss"

                6.12.3 Intrados

		6.12.4 Singular points-segments
		6.12.5 Draw holes
                       Type 1 (elliptical)
                       Type 3 (triangles)
		       Type 4 (rectangles)
		6.12.6 Draw nylon rods - joncs
        	6.12.7 Draw mylars

	6.13 Airfoils drawing (MC mesa de corte)
		6.13.1 Borders
		6.13.2 Singular segments
		6.13.3 Ellipticall holes

 5+. DRAWING REAL WING

	5+.1 Drawing planform in 2D view x-y
		Ribs
		TE
		LE
		Vent in
		Vent out
	5+.2 Drawing real canopy in 2D view x-z
        5+.3 Drawing real canopy in 2D view y-z

 7. PANEL DEVELOPMENT

	7.1 Panel 1'-1 extrados
        7.2 Panel 1'-1 intrados
		7.2.1 Intrados
		7.2.2 Vents calculus and drawing

	7.3 Panels 1 to nribss-1 extrados
	7.4 Panels 1 to nribss-1 intrados
		7.4.1 Intrados
		7.4.2 Vents calculus
                7.4.3 Vents drawing (classic)
		7.4.4 Vents drawing AD

 8. SKIN TENSION

	8.1 Previous calculus

		8.1.1 Extrados longitud cella extrema
		8.1.2 Intrados longitud cella extrema
		8.1.3 Lengths extrados
		8.1.4 Lengths intrados
		8.1.5 Longitud inlet
		8.1.6 Points de calcul amples de celles
	
	8.2 Sobreamples extrados

		8.2.1 Sobreamples esquerra extrados
		8.2.2 Sobreamples dreta extrados
                8.2.3 Reformat right side of the panel (optional)
                8.2.4 Reformat panels for perfect matching

                      Compute rib and panels lenghts
                      Identify points jirl and jirr
                      Reformat left side
                      Reformat right side
                      Final verification
                      Distorsion calculus
                      Distorsion correction

                8.2.5 Calcule external points 11 12 14 15 24 25 26 27
                      Case tangent or orthogonal

		8.2.6 Draw sobreamples panels extrados (Box 1,3)
                      Marks miniribs - minicabs

		8.2.7 Draw panels AD  (Box (1,5)

        8.3 Sobreamples vents
		8.3.1 Vents sobreamples esquerra
                8.3.2 Vents sobreamples dreta
                8.3.3 Corners vents
                8.3.4 Draw vents
                
	8.4 Sobreamples intrados

		8.4.1 Sobreamples esquerra intrados
		8.4.2 Sobreamples dreta intrados
	        8.4.3
                8.4.4 Reformat panels for perfect matching
		8.4.5 Cantonades 26 i 27 intrados
		8.4.6 Draw sobreamples panels intrados i
		vores de costura
                      Marks miniribs - minicabs
		8.4.7 Draw panels AD

       8.5 Draw all panels (using subroutines)
		8.5.0 Launch 3D-shaping calculus and subrutines
			8.5.0.1 Launch 3D-shaping calculus
                        8.5.0 >>> 6.12.0 Miniribs here
                        8.5.0.2 Call tessellation calculus
			8.5.0.3 Draw ovalized airfoils in 2D
       		8.5.1 Extrados without vents
		      Print panel numbers (test)
        	8.5.2 Extrados with vents
        	8.5.3 Vents amb vores
        	8.5.4 Intrados without vents
        	8.5.5 Intrados with vents

       8.6 Draw all panels (with 3D cuts)

                Case k29d=1 then

                8.6.1 Extrados
                Draw minirib extrados
                Case extrados 0 cuts
                Case extrados 1 cut
                Case extrados 2 cuts

                8.6.2 Intrados
                Draw minirib intrados
                Case intrados 0 cuts
                Case intrados 1 cut

 9. SINGULAR RIB POINTS

	9.1 Compute anchor points
        9.1+  Detecta punts j a extrados propers a ancoratges
        9.1++ Detecta punts j a intrados propers a ancoratges

	9.2 Compute inlet points
	9.3 Draw anchor points
		9.3.1 Anchor points
		9.3.2 Anchor points MC
	9.4 Draw inlets
		9.4.1 Cases 0,-1,-2,-3,-4 draw normal inlet LE
		9.4.2 Case 4, draw special displaced LE inlet
        	9.4.3 Cases 0,1,-3,4 draw normal TE inlet
		9.4.4 Case -4, draw special displaced TE inlet
        9.5 Aditional rib points (junquillos)


 9.9 MIDDLE PANEL UNLOADED RIBS

        9.9.1 Define intermediate airfoil
        9.9.2 Compute external edges
        9.9.3 Print internal line
        9.9.4 Print expernal line
        9.9.5 Draw romano and itxt
        9.9.6 Draw vents
        9.9.7 Marks extrados
        9.9.8 Marks intrados
        9.9.9 Draw holes
        9.9.10.1 Draw equidistant points extrados
        9.9.10.2 Draw equidistant points intrados

 10. CALAGE

	10.1 Basic calculus
        10.1+ Angle beetween glidepath and airfoil plane
	10.2 Karabiners location
	10.3 Calage drawing
		Central airfoil
		Chord
		Pilot-CP and Pilot-C
		Assiette ans AoA angles
                Write text in dxf file

 11. CALCULE LENGTHS EXTRA INTRA EN PANELLS I PERFILS. MARKS

 	11.1 Calcula lenghts and amplification coefficients
             - Old system
             - New system
	11.2 Lenght verification (no used)
 	11.3 Rib marks
                11.3.1 Extrados
                11.3.2 Intrados
                       case "ds" or "pc"
 	11.4 Panel marks

		11.4.1.1 Extrados
		11.4.1.2 Extrados left
		11.4.1.3 Extrados right

		11.4.2.1 Intrados
		11.4.2.2 Intrados left
		11.4.2.3 Intrados right
                11.4.2.4 Roman numbers in intrados
                11.4.3 Anchor marks in intrados panels

 12. LINES CALCULUS

	12.1 Matrix de cordes
	12.2 Identifica cordes a calcular
             Set lines types
	12.3 Compute anchor points in 3D space
	12.4 Compute singular rib points in 3D space (brakes, inlet in, inlet out)
        12.4+ Redefine virtual anchor points in extrados for "ss"

            Option to modify rib for PAMPAlike sk

        12.4++ Compute load in each anchor
	12.5 Lines d'accio of each corda
	12.6 Points inicial i final of each corda
             Calcula angles a girar "ss" phi0=phi1-phi2
		12.6.1 Level 1: Risers
	        12.6.2 Level 2
		12.6.3 Level 3
		12.6.4 Level 4
	12.7 Rotate triangles in 3D, only "ss"

             Option to modify rib for PAMPAlike sk

	12.8 Lengths de les cordes
        12.9 Corrections elastiques
        12.10 Draw cordes 2D

 14. BRAKE CALCULUS

	14.1 Matrix de cordes
	14.2 Identifica cordes a calcular
             Set lines types
	14.3 Compute anchor points in 3D space
	14.4 Lines d'accio of each corda
             Recompute fractional anchors
	14.5 Points inicial i final of each corda
		Level 1
		Level 2
		Level 3
		Level 4
	14.6 Lengths de les cordes
	14.7 Draw brakes 2D

 15. COLOR MARKS

     15.1 Extrados marks
     15.2 Intrados marks

 16. H V AND HV RIBS

	16.1 H straps (Type 1)
		16.1.1 Line i
		16.1.2 Line i+1
		16.1.3 Lines 2 and 3 transportation on the space
		16.1.4 H-rib 2-3 in 2D model
			Calculus
			Drawing
			Numering

	16.2 V ribs partial (Type 2)

		16.2.1 Rib i
		16.2.2 Rib i-1
		16.2.3 Rib i+1
		16.2.4 Lines 1 2 3 transportation on the space
		16.2.5 V-ribs calculus and drawing
			V-rib 1-2 in 2D model
			V-rib 2-3 in 2D model
			V-ribs in 2D ribs

       	16.3 V ribs full (Type 3)

                16.3.1 Independent diagonal strips (Type 3)
                       16.3.1.1 Rib i points 2,3,4 and reformat
                       16.3.1.2 Rib i-1 points 9,10,11 and reformat
                       16.3.1.3 Rib i+1 points 9,10,11 and reformat
                       16.3.1.4 Lines 1 2 3 transportation to 3D espace
                       16.3.1.5 V-rib flat calculus and drawing in 2D
                       16.3.1.5.1 Compute and draw 1-2 rib
                       16.3.1.5.2 Compute and draw 2-3 rib
                       16.3.1.5.3 Drawing V-ribs marks in 2D ribs

                16.3.2 Continous full diagonal ribs (Type 5)
                       16.3.2.1 Rib i points 2,3,4 and reformat line 2
                       16.3.2.2 Rib i-1 points 9,11 and reformat line 1
                       16.3.2.3 Rib i+1 points 9,11 and reformat line 3
                       16.3.2.4 Lines 1 2 3 transportation to 3D espace
                       16.3.2.5 V-rib flat calculus and drawing in 2D
                       16.3.2.5.1 Compute and draw 1-2 rib (blue)
                       16.3.2.5.2 Compute and draw 2-3 rib (red)
                       16.3.2.5.3 Drawing V-ribs marks in 2D ribs

	16.4 HV ribs (Type 4)
		16.4.1 Rib i-1
		16.4.2 Rib i
		16.4.3 Rib i+1
		16.4.4 Rib i+2
	16.4.4 Lines 1 2 3 4 transportation on the space
	16.4.5  VH-ribs calculus and drawing in 2D and 3D
		VH-rib 1-2 in 2D model
		VH-rib 3-4 in 2D model
		VH-rib 1-3 in 2D model
		Drawing VH-ribs in 2D ribs

        16.6 V ribs Type 6 "general"
     
                16.6.1 Rib i points 3,2,4,6,8,9,11 and reformat
                16.6.2 Rib i+1 points 3,2,4,6,8,9,11 and reformat
                16.6.3 Lines 2 3 transportation to 3D espace
                16.6.4 V-rib flat calculus and drawing in 2D
                16.6.5 Drawing V-ribs marks in 2D ribs
                       Rib i   (tree cases)
                       Rib i+1 (tree cases)
                16.6.6 Drawing V-ribs Type 6 in 3D model

 17. CALAGE CALCULUS


 18. TXT OUTPUT lep-out.txt
	18.1 Main
        ADJUSTEMENT SEAM PARAMETERS
        DISTANCES ENTRE ANCORATGES
        18.2 Adjustement seam parameters
	18.3 Speed and trim calculus
		18.3.1 a) Speed system pivot in last riser
		18.3.2 a) Speed system pivot in first riser
		18.3.3 a) Trim system pivot in first riser
		18.3.4 a) Trim system pivot in last riser
                18.3.5 Draw calage variations in dxf
	18.4 Print joncs
        18.5 Print 3D-shaping details
        18.6 Print extrados and intrados informative coefficients k
        18.7 Print information about profil points
        18.8 Print angles between airfoil plane and glidepath
	18.9 Risers information
	18.10 Lines characteristics table
	18.11 Solve equilibrium equations
	18.12 Some parameters used in XFLR5 analysis
        18.14 Some special parameters


 19. lines.txt List of lines in human readable format

 20. Draw labels in 2D (in tree of lines)

 21. 3D DXF MODEL DRAWING

	21.1 Extrados
	21.2 Vents
	21.3 Intrados
	21.4 Trailing edge
	21.5 Leading edge (in/out)
	21.6 Lines 3D
	21.7 Brakes
	21.8 H-V-ribs 3D drawing
		21.8.1 H-ribs
		21.8.2 V-ribs partial
		21.8.3 V-ribs full
		21.8.4 VH-ribs
        21.9 Intermediate and ovalized airfoils
        21.10 Draw DXF tessellation in 3D model
        21.11 Draw DXF tessellation in 3D external file lep-3d-surfaces.dxf
        21.12 Draw SCAD tessellation in 3D external file (OpenSCAD file) lep-3d-surfaces.scad
        21.13 Draw STL tessellation in externel file lep-3d-surfaces.stl

 22. TEXT NOTES IN BOXES

     22.1 (Text in boxes)

     22.2 Write lines in plan A, B, C, D, E, F

 23. END OF MAIN PROGRAM

 24. SUBROUTINES

 SUBROUTINE POINTG

 SUBROUTINE POINT

 SUBROUTINE POINC (used?)

 SUBROUTINE POINL (used?)

 SUBROUTINE CIRCLE

 SUBROUTINE MTRIANGLE

 SUBROUTINE LINEVENT

 SUBROUTINE SEGMENT101

 SUBROUTINE LINE

 SUBROUTINE LINE3D

 SUBROUTINE POLY2D (not used)

 SUBROUTINE ELLIPSE
 
 SUBROUTINE ROMANO

 SUBROUTINE TEXT

 SUBROUTINE ITEXT

 SUBROUTINE DXFINIT

 SUBROUTINE DXFEND

 SUBROUTINE VREDIS vectors redistribution

 SUBROUTINE XRXS r and s lines 2D intersection

 SUBROUTINE FLATT FLATTENING

 SUBROUTINE axisch

 SUBROUTINE angdis2 (experimental)

 SUBROUTINE d3p (no imp)

 SUBROUTINE extpoints extrenal points in a panel 

 SUBROUTINE dpanelc

 SUBROUTINE dpanelcc (with control)

 SUBROUTINE arc3p

 SUBROUTINE drwvent , draw vent types, with control



 SUBROUTINE dpanelc1

 SUBROUTINE dpanelc2

 SUBROUTINE dpanelcm2

 SUBROUTINE dpanelcm3

 SUBROUTINE dpanelb

 SUBROUTINE dpanelb1

 SUBROUTINE dpanelb2

 SUBROUTINE joncs

 SUBROUTINE interpola(x1,y1,x2,y2,x3,y3)

 SUBROUTINE interpd(x1,y1,x2,y2,x3,y3,xd)

 SUBROUTINE pjoncs(i,xjonc,npo,sjo,sepx,sepy,rib,xkf)

 SUBROUTINE loffset(uo,vo,npo,xo)

 SUBROUTINE puntslat


 SUBROUTINE mylars(i,u,v,sepx,sepy,rib,xmy,np,xkf,atp)

 SUBROUTINE interpolyg , polyline linear interpolation

 SUBROUTINE lagrangeip , polyline Lagrange interpolation

 SUBROUTINE fletxa , haut of a circular segment (WARNING used?)
 
 SUBROUTINE panels3d , main 3D calculus

 SUBROUTINE czinf , compute zones of influence of cuts

 SUBROUTINE planeby123 , plan ABCD by points 1,2,3

 SUBROUTINE unitaryto123, unitary vector and normal to plane by 123

 SUBROUTINE pointp3d , point by 0 perperdicular to plan ABCD at d

 SUBROUTINE glo2loc , transform global 3d coordinates to local

 SUBROUTINE print01 , print TE extrados


 SUBROUTINE prinifp , print initial and final points r panel

 SUBROUTINE prinfpv , print final points vents

 SUBROUTINE llarlr , computes length alt left and right

 SUBROUTINE xmarksi , marks at left and right panel

 SUBROUTINE iam , intrados anchor marks

 SUBROUTINE romanop , romano point in line 1-2

 SUBROUTINE romanoparc , romano point in arc in a panel uf,vf



 SUBROUTINE datair, reformat dat airfoils (NOT FINISHED)

 SUBROUTINE remapcontour, (NOT FINISHED)

 SUBROUTINE xyzt, Rotates points in airfoils in tree axes and moves to absolute ccordinates

 SUBROUTINE elliquad, Draw ellipses inside quadrilaters P1-P2-P3-P4

 SUBROUTINE distpr, Distance between point P3 and line r (P1-P2)

 SUBROUTINE arcfle, Draw arc between points P1-P2, arrow, sign, color



 SUBROUTINE interpoly2d

 SUBROUTINE interpoly3d

 SUBROUTINE eo (even odd detection)

 SUBROUTINE distanceabc  Calcules point 3 at a distance from 1, in segment between points 1 and 2

 SUBROUTINE tessella(x1,y1,z1,x2,y2,z2,x3,y3,z3,distance)

SUBROUTINE interpseg(jini,jfin,jc,ldif,
     + useg,vseg,ltotal,linter,upoint,vpoint) > polyline interpolation


SUBROUTINE loc2glo2D(n,xloc,yloc,xglo,yglo,x0,y0,angle)
Local to global coordinates 2D by translation and rotation




