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STRESS-STRAIN RIPSTOP CURVES (II)
Effect of the bias in grid angle
By Eric Fontaine

1. Introduction
2. Practical tests
3. Stress-strain curves
4. Conclusions
5. Videos

1. Introduction

This experiment has been carried out by Eric Fontaine in may of 2021. Some comments added by Pere Casellas. It complements the experiments carried out previously on the deformation of ripstop samples under increasing load.

The objective of this experiment is to study the deformation of ripstop samples with different grid angles. It is well known that the deformation of the ripstop in bias directions, is greater than the deformation in directions parallel to the main grid. Here, we measure and quantify this effect. This deformation has importance in different aspects of the design of the structure of the paragliders. In particular, in a single skin, a poor design that does not take into account these effects, may cause excessive deformation in profiles and loss of performance, due to not foreseen deformations in the load triangles.


Test device

Fig 1. Testing device
samples
Fig 2. Ripstop samples plan. Samples at 0, 30, 45 and 60 degrees.
0 in the transverse direction "weft" (or "woof")


The test system consists of loading progressively a ripstop tissue strip of 5 cm wide, and simultaneously measuring the distance between two reference points marked on the tissue, and the applied load. The load is increased gradually from 0 kg up to 6 kg.

The result is a table with the pair of values (distance (mm), load (kg)).
For a stress-strain curve normalized, these values are converted as follows:

Stress (kg/cm) = Load (kg) / 5 cm
Strain = ( (Distance / Initial distance) ) -1 )



2. Practical testing

Some photographs taken during the tests:


4. Preparation of samples for cutting with laser.

5. Samples
3
6. Sample detail
4
7. Samples using Skytex 40 gr hard finish


3. Stress-strain curves

Data sheet (format openoffice).

results
For each measurement angle, two experiments have been performed, presenting the average result in the table.

4. Conclusions

- The deformations at 45 are more than three times greater than the deformations obtained at 0
- The deformation obtained at 30 is slightly lower than that obtained at 60. This is consistent with other experiments carried out previously, according to which the deformation in the sense of the weft (transverse) is lower than in the warp (longitudinal)
- The permanent deformation (after removal of the load) is much higher in samples loaded at 45
- It is recommended to design the triangles of support of single skin wings to avoid deformations differential. The same applies to diagonal V-ribs in the interior of double surface paragliders.


5. Videos:

Test (part I):




Test (part II):

 


Read more: STRESS-STRAIN RIPSTOP CURVES (I) and Ripstop elasticity

Note: The data presented here are not official, and do not represent the average characteristics of the tissues.

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