1.1 Introduction
1.2. Geometric Definition
    1.2.1 Analytical methods
    1.2.2 Discrete method
1.3 Center of gravity

2.1 Introduction
2.2 Cylinder in an airflow
2.3 Joukowsky transformation
2.4 Airfoil geometry and parameters
2.5 Aerodynamic forces
2.6 NACA profiles
2.7 Paraglider airfoils
2.8 XFOIL program
2.9 XFLR5 program
2.10 AIrfoil fitting

3.1 Main lobe "voute"
3.1 Influence of the shape of the lobe
3.3 Geometric torsion (washin)
3.4 Profil insertion

4.1 Introduction and definitions
4.2 Equations of static equilibrium
    4.2.1 Sum of moments from a  point is equal to zero
    4.2.2 Sum of vertical forces is zero
    4.2.3 Sum of horizontal forces is zero
4.3. Solving the system
4.4. Spreadsheet
4.5. Simplified equilibrium aproximation
4.6. Empirical methods
4.7 Adjusting the speed of a prototype

Longitudinal equilibrium in 2D, Considerations 3D, Aerodynamic twist in the wing (washout), Trimming, Calage

5.1 Introduction
5.2 Description of the LE method
5.3 Analytical geometry principle
5.4 The FORTRAN subroutine

6.1. Introduction

6.2 Analysis of the ovalization in transverse direction to the cells
6.3 Analysis of the ovalization along the axis of the cells
6.4. Corrections to the panels

8.1 Geometrical design
8.2 Brakes and brake distribution
8.3 Elasticity
8.4 Loads

9.1 Introduction
9.2 Analysis of 4 riser speed system
9.3 Trimmers
9.4 Vario seat

Nylon ripstop
Polyester ripstop
Mylar
Dacron
Aramide
Dyneema
Maillon
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