MORE PHYSICS
During the inflation process there are very strong dynamic forces, among which the
aerodynamic drag plays an important role. The amount of these forces and the size
and shape of the payload determines the speed of terminal descent. The payload is
ideally an axial-symmetric slender body.
Large non symmetric bodies create a wake flow that interferes with the air captured
by the canopy, either slowing the inflation process or creating an unsymmetric
situation wherein the operation is compromised.
The deformation of the canopy creates a strongly non linear interaction between the
aerodynamics and the structure. The aerodynamics is that of a bluff body, which is
one of the most difficult problems in terms of quantitative prediction.
The sinking speed (or rate of descent) U depends on the drag
coefficient, on the frontal area of the canopy and the total weight of the parachute. In a vertical descent it is simply a balance between the aerodynamic force (upwards) and the
wight (downwards).
Selected References
- Hoerner SF. Fluid Dynamic Drag, Hoerner Fluid Dynamics, 1965 (Chapt XIII)
- AGARD, Design and Testing of High Performance Parachutes, AGARD AG-319, 1991.
- Cockrell, J. The Aerodynamics of Parachutes, AGARDograph No. 295,
- Smith IS, Cutts JA. Floating in Space, Scientific American, Nov. 1999.
- Peterson CW. High Performance Parachutes Scientific American, May 1990.
There is a number of publications dealing with paragliding and other aviation
sports. For specific references, please inquire.
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