Definite Integrals: Application to Paragliding

Dr. Gottfried Mayer

http://www.santafe.edu/~gmk/PG/Wing, gmk@santafe.edu

Paragliders are like modern parachutes that are designed for best gliding properties. Therefore they are not used from airplanes but pilots launch from hills or mountain slopes. In good weather conditions they can stay aloft for hours and can travel for ore than hundred miles. They have a single wing that is inflated when air enters through openings in the front ("ram-air" system).

 

The size of the wing determines how much weight the wing can cary. To be more specific: The "projected area" of the wing that means the area that is horizontal and therefore providing "lift". In this example we want to calculate the area of a paraglider wing from its (projected) wingspan and its "aspect ratio".

 

The above drawing shows the projected area of a modern paragliding wing. Its technical data are given in the table below.

Projected wingspan 2a

11.03 m

Projected aspect ratio r

4.37

Legal take-off weight m

100-130 kg

Determine the Projected Area of the Wing:

  • Approximate the wing shape by two ellipses of semi major axis a and semi minor axes b1,b2 with b1+ b2 = 2 a/r and b1/b2 =1.5
  • The equations for each of the semi ellipses can be derived by solving the defining equation:

    for y:

     

    Problems:

     

    Notes: