FAQ version 2.40 updated 5 september 2015

LEparagliding is a very powerful program used to design paragliders and parachutes. The program is fully functional and has no restrictions on its use. First, it is necessary to read the latest version of the manual, in its versions in English or Russian. In this FAQ, clarified some aspects. If you need further clarification, write to info @ laboratoridenvol com

1. Running LEparagliding

1.1 How
to run leparagliding?
1.2 Why is it so difficult to use leparagliding? There could be more easy?
1.3 I can run LEparagliding on MAC OSX?
1.4 DXF format and CAD programs


S1.1 Drawing "scale" parameter in SECTION 1.
S1.2 Wing scale parameter in SECTION 1.
S1.3 In SECTION 1, What effect does the second parameter?, boolean 1 or 0?
S1.4 "Rib geometric parameters" (x-rib, y-LE, y-TE, xp, z, beta, ...)
You can put a simple example?
S1.5 Rib geometric parameters, how to calculate the "beta" angle?


S2.1 In SECTION 2, What effect does the parameter "displacement in cm" in the sixth column of the blog
S2.2 In SECTION 2, What effect does the parameter " Relative weight of the chord, in relation to the load" in the seventh column of the blog


See pre-processor



1.1 How
to run leparagliding?

11) Download the latest version in a .zip package here: leparagliding2.40.zip

2) Unzip leparagliding2.40.zip. You will see a folder with the following files:


Note that leparagliding.txt contains the design of an example paraglider. There is not a real design, is intended only to show the possibilities of diagonal ribs type 5.
paragliders BHL3 gnuLAB4 and will be designed with this version.

3) The program is ready to run because leparagliding not need installation. Simply copy the folder and its content to your working directory.

4) Running the program:

4.1) In GNU/Linux systems:

Open a shell (xterm, kconsole...) and cd into the folder leparagliding2.40
Execute the program typing ./lep-2.40.out
After a few seconds, if all goes well, the console outputs OK and some new files are created in the same directory with the results of the program:


4.2) In WIndows systems:

Double Click in e.exe, and after a few seconds, some output files (.dxf and .txt) should appear in the same working folder.

5) That's it! Nothing spectacular! The plans are in 2D format in file leparagliding.txt and in 3D in file lep-3d.dxf. Is need a powerful dxf file editor program. This can be a major difficulty if you are not accustomed to working with CAD files types dxf / dwg. DXF format is used to work very precisely and make small changes and improvements on plans obtained. It is also used to prepare PDF files for printing, or create DXF / DWG for use in a computerized laser cutting table. Files lep-out.txt and lines.txt contains a summary of the technical parameters of the wing and the list of lines with their lengths. And you can open with any text editor. The difficulty of the design is to correctly understand and write the data file leparagliding.txt and associated profiles files. Please, study the manual.

Note: current executables only for 32-bit. Soon also compiled for 64-bit. However the ideal is that you compile yorusefl in yor machine using gnufortran compiler.

2. Why is it so difficult to use LEparagliding? There could be more easy ?

it would be possible in the future to make a GUI (
graphical user interface) to write file leparagliding.txt and profiles, graphically and interactively. But this requires a great deal of programming and now we prefer to concentrate on the content and the proper functioning of the geometry routines. Write leparagliding.txt file is much easier than programming a GUI. Also, I find more neat and orderly easily write data in file leparagliding.txt that through a bunch of menus.

On the other hand, before writing the data, pre-processing work is essential, then run the program, then a post-processing work. The pre-processing and post-processing parts are very important for good design.

(... to continue and explain better pre and post-processing)

3. I can run LEparagliding in MAC OSX?

Yes, of course. Some have done successfully. Source code file leparagliding.f is written in "gnu Fortran". Just install a Fortran compiler. Install gcc, F77, F95 or similar to your computer.


Drawing scale parameter in SECTION 1.

Drawing scale (1.0) is the usual value. Is a drawing parameter that does not affect the design, only the graphic representation of plans. If the “drawing scale value” is set to 1.0, then the size of the rectangular boxes that outline each of the plans, is exactly 1260 units (cm) horizontally and 891 units (cm) vertically. These measures are arbritaries, and have been chosen in order to represent a wing with span less than 12.6 meters. The vertical dimension is in the ratio (1/sqrt(2)) characteristic DIN sheets of A4 or A3 size. If you design a wing with span greather than 12.6 m, a wing or two-seater, or with a large number of cells, then you need to increase the scale of the box, for example 1.5 value (box 1890 cm x 1336.5 cm). If you draw a speed glider, perhaps you can use a parameter like 0.8

S1.2 Wing scale parameter in SECTION 1.

Wing scale (1.0) is the usual value. Is a design parameter. If you design a wing with this setting specified in 1.0, you get a wing size “M” of surface “A” in m2. If you want to make another wing of the same model but different size, just you need change this setting, leaving all others unchanged. For example, for size S, you can use the parameter 0.95 and the new surface is A x (0.95)^2. For a size L, you can use a parameter 1.05 and the new surface is A x (1.05)^2.

This parameter “k” is also explained here:


S1.3 In SECTION 1, What effect does the second parameter?, boolean 1 or 0, in the line that says:

text, boolean : Paraglider type "ds", "ss", or "pc", and parameter set to 0 or 1. If "1" then leading edge triangles will be no rotated (only ss paragliders)

In order to correctly calculate the lengths of the lines, in single skin gliders, the triangles are automatically aligned in the same direction of the forces of traction of the top lines. Indeed, according to the distribution of the ramifications of the top lines, there are some lines that tension in converging directions, and others in diverging directions. But the lines anchored in the “A” row (leading edge) do not cause rotations in profiles, because the small area of soffit (bottom surface) prevents it. It would be possible to rotate profiles in row “A”, but it is very rare design. This parameter leave the freedom to do it or not by the designer. See figure “Rotated triangles.jpg”.

A new feature in 2.35 version (not documented before), prevent rotation of all triangles in specified ribs. This is useful for special line designs like BHL-Pampa.

rotated triangles

Rotated triangles

S1.4 "Rib geometric parameters" (x-rib, y-LE, y-TE, xp, z, beta, ...) You can put a simple example?

Yes, look here: Simplified.dxf

For example, paragliding 6 profiles (not a realistic model)

First, it is necessary to draw the shape of the wing (plan view in axes X-Y, front view in axes X'-Z). Take into account the orientation of the axes. It is obligatory to do so before starting to work with the program. It is better to draw using AutoCAD or similar programs. But it can also be in old style with graph paper and a pencil (also the result will be perfect, because you will be obtained numerical coordinates). Then it is necessary to measure the coordinates of the main points of the edge, the trailing edge and the frontal arc. We must also measure the angle beta.

This may seem laborious, and it is. But it is very important. The pre-processor program, helps greatly to do that.

S1.5 Rib geometric parameters, how to calculate the "beta" angle?

Consider the scheme of the wing, in a front view (see Figure below):

- Profiles, in blue
- The main axis of the arc of the wing, in the red
- Draw a vertical line at the point of intersection between the profile (blue), and the main axis of the arc of the wing (red)
- The angle beta, is by definition the angle between the profile lines and the vertical reference line.

Geometrical conditions to be considered is that the profiles are taken (usually), perpendicular to the reference axis red (the arc of the wing). That is, 90 degrees between the red and blue line. This condition is not mandatory. That is, it was possible to make profiles with angles other than 90. However, in the central part of the wing, it is better to make them perpendicular 90 degrees.


S2.1 In SECTION 2,
What effect does the parameter "displacement in cm" in the sixth column of the blog ?

See attached figure “delta displacements.jpg”. The wing is designed basically putting profiles into space, and then calculating and obtaining the shape of the panels in top and bottom surfaces.

- The theoretical situation would be that is shown in Figure 1.

- But the experimental result is always shown in 2. Profiles without lines are misaligned with respect to the loaded. Due to the distribution of forces.

- One option is perhaps force the misalignment of not loaded profiles with a shift “delta” ialong the  "Z" axis as shown in Figure 3. Calculated shape of the panels would be ideal for this form.

- The experimental result should be shown in Figure 4, all aligned profiles.

Though this theory I have not been able to experiment with sufficient detail. At first glance, Figure 3, seems to cause an effect completely opposite to the expected (even more distortion than figure 2). In short, this is an experimental parameter, and if in doubt, leave the delta displacement at 0 cm. To limit the movements in not loaded profiles, the solution are the diagonal ribs.


Relative delta displacements in "Z" axis

S2.2 In SECTION 2, What effect does the parameter " Relative weight of the chord, in relation to the load" in the seventh column of the blog

To calculate the alignment of the lines in space, LEparagliding use the theory consisting of align with the center of gravity of the anchor points corresponding of each line (or riser). The simplest solution to get the center of gravity of n points in space is to get each of the coordinates x, y, x as arithmetic mean: sum of each of the values ​​divided by the total number of values. This would be correct if each anchor point support it exactly the same load. But it is not. Therefore, the program uses a weighted average, considering a load distribution in % in A, B, C, D, E. .. and also the length of the airfoil chord. I think I have to explain this in more detail. It is possible to manually assign relative weights of each rib. This parameter allows the designer manually assign relative weights of each rib. It is an advanced parameter, which is not yet fully implemented.



Panel formation
The program (version 2.35 or fewer) draws the panels in three parts:

- Extrados (upper surface)
- Panel to close inlets
- Intrados (bottom surface)

Panels inlets, are drawn without seam edges added.

In general, if the air intakes are designed open (normal), no need to consider these panel. But if some cells are considered closed (for example, near the wing tips), you need to add these panels to the design.

In double surface paragliders, these panels can be added at the Intrados panel using the CAD program.

In single skin paragliders,
is practical, consider all the air intakes "closed", and add (using CAD) these panels to the top surface, thus forming part of the monolayer single skin. This is how the BHL's models were made.

This is part of the "post-process" on the plans in CAD format (DXF).

Using CAD, it is possible to cut circular holes, elliptical, or any form of cuts, on inlet panels, to create special shapes.