CONCEPTION OF CRASH TESTS FOR COMPOSITE TUBULAR STRUCTURES H. Zabala - - PDF document

conception of crash tests for composite tubular structures
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CONCEPTION OF CRASH TESTS FOR COMPOSITE TUBULAR STRUCTURES H. Zabala - - PDF document

18 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS CONCEPTION OF CRASH TESTS FOR COMPOSITE TUBULAR STRUCTURES H. Zabala 1 *, J. Aurrekoetxea 1 , M. Mateos 1 , G. Castillo 2 , L. Aretxabaleta 1 1 Mechanical Engineering and Industrial


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SLIDE 1

18TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS

Abstract

A lot of research work on geometrical, material and loading factors’ influence on composite tubular structures behaviour under crash conditions has been undertaken. Most of these works have dealt with tubular structures subjected to compressive loads, which can induce local buckling phenomena. Under these conditions only a small amount of material is degraded resulting in a small energy dissipation level in a non-controlled way. The tests proposed in this communication allow measuring the crashworthiness of tubular structures for the automotive industry subjected to different contour conditions. Three different initiator plugs have been proposed to carry out the compression tests: flat, conical and radial ones and tests at different strain rates have been performed. For the selected initiators dimensions, no influence of the strain rate on the dissipative behaviour of compressed carbon- epoxy 0/90 tubes has been observed.

  • 1. Introduction

Composite structures have been widely used to produce energy dissipation during a crash [1-3]. Energy is dissipated through damage mechanisms that include intra- laminar failure (fibre and matrix rupture) and inter- laminar failure (delamination). There are several numerical approaches to predict the complex damage behaviour of composites, like Hashin’s damage initiation and degradation model [4]; nevertheless, the information needed to feed these models in a reliable way is often difficult to get through non standard tests carried out at conditions different from the ones that happen in real life (i.e. quasi static tests for feeding crash models). The most common way of dissipating high amounts of energy is to subject the structure to a compressive load high enough to produce the crushing of the structure [5- 8]. Different configurations of tubular structures [9-13] or tests [14-15] have also been studied in order to obtain higher energy dissipation. In some cases, the goal can be to get the energy dissipation in a more controlled way. One of these test configurations consists in the use of different shape plug initiators like radius or cone shaped plugs. Most of these experimental works are carried out in quasi- static conditions, but most of the real life applications of energy dissipation structures occur at impact velocities and/or energies. The dependence of energy dissipation capabilities on strain rate has been reported in a few works, as for example in [16], where rectangular section 3D braided E-glass/epoxy composites have been crushed at different strain rates, showing a clear higher energy absorption capability as strain rate increases. The aim of this work is to develop an experimental test methodology that will allow testing tubular composite structures at different strain rates (from quasi-static to low velocity impact) and different boundary conditions (with different shape plug initiators). The objective is to be able to get information about the material damage behaviour in different conditions that will allow validating existing damage initiation and degradation models. In this communication only the preliminary results of this work are shown.

  • 2. Material and experimental test

2.1. Material

Tubular structures of two different materials have been used in this study. In the first step, with the aim of

  • ptimizing the testing equipment and plug initiators, a

commercial non reinforced PVC straight pipe with an

  • uter diameter of 40 mm and 3.2 mm thickness has been
  • used. Specimens were cut at lengths of 40, 60 and 80 mm.

Testing tools with different geometries have been built for analyzing their influence on the crushing behaviour of the PVC pipes. The second structure has been a commercial pultruded unidirectional carbon fibre composite pipe, with an outer

CONCEPTION OF CRASH TESTS FOR COMPOSITE TUBULAR STRUCTURES

  • H. Zabala1*, J. Aurrekoetxea1, M. Mateos1, G. Castillo2, L. Aretxabaleta1

1Mechanical Engineering and Industrial Manufacturing Department, Mondragon Unibertsitatea,

Mondragon, Spain

2Civil, Materials and Manufacturing Engineering, University of Malaga, Malaga, Spain

* Corresponding author (hzabala@eps.mondragon.edu)

Keywords: Crash, composites, crashworthiness

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SLIDE 2

a th m F m

  • 4

th

2

T su 1 m te b a fl ( T m 1

3 3

T st d th fa b 0/90 fabric lay an outer diame his case, all t mm. Finally tubes made by hand

  • f a 0/90 fabri

40 mm and 2. he samples ha

2.2. Quasi-st

The tests met upported by d ). The tests machine config est configurat between flat p and a conical t flat plate and a (a) Figure 1: Rep (a) Flat plates (c) f Tests have be mm/min for P 20 and 480 m

  • 3. Results an

3.1. Tests on

The tests on PV tructures are depending on here was no failure behavio buckling phen

  • yer. The dime

eter of 40mm the specimens

  • f 0/90º wov
  • lamination. A

ic layup was b .2 mm thickn as also been 50

tatic compre

thods consist different initia are carried o gured in comp tions have bee plates, b) com tool (α=55º) a a radial tool (R ( presentation o , (b) flat plate flat plate and r een performed PVC specimen mm/min for the

nd discussion PVC tubes

VC samples h subjected to the initiator p influence of

  • ur, since it w

nomenon in ensions of the m and a thickn s have the sa ven carbon f A tubular stru built with an i

  • ess. In this ca

0 mm.

ession tests

in compress ator plugs in th

  • ut in a univ

pression mode en performed: mpression betw and c) compre R=22 mm). (b) f the develope and conical p radial plug ini d at a consta ns and at test e carbon fibre

n

have demonstr a very diffe plugs used. I f the sample was a conseq the three tubes have b ness of 2 mm ame length of fibre-epoxy w ucture of 8 lay inner diamete ase the length sing the samp heir bottom (F ersal tensile

  • e. Three differ

: a) Compress ween a flat p ession betwee (c) ed test method plug initiator a itiator. ant velocity o t velocities o e-epoxy ones. rated that tubu erent stress s t was found t length on f quence of a lo cases (Fig. been

  • m. In

f 50 were yers r of h of ples Fig. test rent sion plate en a ds: and

  • f 1

f 1, ular state that final

  • cal

2). Ne at thr ini con bot fla Fi Fla Fig p Fro for rad in hig ini

  • cc

it i stru Th to Th evertheless, th different stag ree cases the tiation of the nfiguration oc th i) the flat p t plate and rad (a) gure 2: Tested at plates, (b) f gure 3: Force- plugs on PVC and conical in

  • m Fig. 3 it ca

rce achieved i dial initiator p a more contro gher for larg tiator plugs curs for a high is possible to ucture once th hese results co improve the c he energy d hese buckling ges of strain, maximum for e buckling fai ccurs for a lo plate and coni dial plug initia (b d samples with flat plate and c and radi

  • displacement

specimens: (P nitiator plug an initiato an be conclud s the same, in plug the energy

  • lled way. It c

ge displaceme due to the f her deformatio avoid the un he first local c nfirm that dif crashworthine dissipation be failure modes as shown in rce value corr ilure, but for

  • w strain leve

ical plug initia ator. b) h local buckli conical tool an ial tool. t curves for di P) Flat plates, nd (R) flat pla

  • r tool.

ded that even i n the tests for y absorption f can be seen th ents in coni fact that buck

  • n of the struc

npredictable be crash is given. fferent initiato ss of tubular P ehaviour of s were achieve n Fig. 3: in th responds to th the flat plat el compared ator, and ii) th (c) ing failures: (a nd (c) flat plat fferent initiato (C) flat plate ate and radial if the maximu the conical an for PVC occu hat this value cal and radi kling thresho

  • cture. This wa

ehaviour of th r plugs are ab PVC structure carbon-epox ed he he es to he a) te

  • r

um nd urs is ial

  • ld

ay he ble es. xy

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SLIDE 3

c a th d d

3

In sh in F In a m W s d th In c w m a c lo m c

  • c
  • F

d fo c composites is v achieved dama he case of P deformation, w due to several

3.2. Tests on

n Fig. 4 tested

  • hown. It can

n any case. (a) Figure 4: Test (b) flat plate n the three ca along the spe mode varies fo When compre ample end damaged; the d he total displa n the case of compression d which open wh mode does no and it is deduc conicity angle

  • ngitudinal cr
  • material. For

created in the

  • ne the openi

cracks; the fina

  • ther end of th

For the conic displacement force and ener configuration ( very different aging the stru PVC the dissi while in carbo damage mech

carbon-epo

d 0/90 carbon be seen that b ( ted 0/90 comp and conical in and radial i ses damage in

  • ecimen. How
  • r each compr

ession betwee where dama damaged mate acement achiev the conical an damage involv hile the displa

  • t allow dama

ced that more e α and rad racks and in the conical sample open u ing is produc al failure occu he specimen. cal and radia curves show rgy dissipatio (Fig. 5). CONCEP t to PVC, but i ucture as muc ipation occur

  • n-epoxy com

hanisms.

  • xy composi

n-epoxy compo buckling failu (b) posite samples nitiator plug a initiator plug. nitiates in one wever, the da ression tool. en flat plates age started erial volume i ved during the nd radial initia ves some lon acement incre aging all the m severe initiat dius R) will consequence initiator plug uniformly, wh ced at the tip urs when this c al initiator p around 70-7

  • n than the cl

PTION OF C in both cases ch as possible rs due to pla mposites it occ

ite tubes

  • site samples

ure is not pres (c) s: (a) Flat plat and (c) flat pla e end and exte amage evolut s is applied, gets complet is proportiona e test. ator plugs, ini ngitudinal crac

  • ases. This fail

material volu

  • r plugs (sma

l produce m , more dama g all the cra hile for the ra p of one of crack reaches plugs, the for 75% lower p lassical flat p CRASH TEST it is : In astic curs are sent tes, ate ends tion the tely al to itial cks, lure ume, aller more aged acks dial the the rce- peak late Fig plu Th uni ver ini pro In car sho the for F rat TS FOR COM gure 5: Force- ugs in 0/90º co he same test idirectional ca ry low energy tiators due to

  • duced and pr
  • Fig. 6 force-d

rbon-epoxy sp

  • wn at differe

e structure sh rce value is low Figure 6: Force tes in unidirec MPOSITE TU

  • displacement
  • mposite sam

mm/m comparison arbon-epoxy y was dissipat

  • the fact tha

ropagated at a displacement pecimen test w ent strain rates

  • ws a higher

wer. e-displacemen tional pultrud conical i UBULAR ST t curves for di mples with a te min. have been specimens, an ted for the con at a longitud very low forc curves for the with the conic s: As the strain r stiffness but nt curves for d ded composite initiator. TRUCTURES fferent initiato est velocity of performed o nd as expecte nical and radi dinal crack w ce level. e unidirection cal initiators a n rate increas t the maximu different strain samples with 3 S

  • r

1

  • n

ed, ial as nal are es um n h a

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SLIDE 4

In Figs. 7-9 the force-displacement curves of tests performed on 0/90 carbon-epoxy composite samples are

  • shown. In this case no influence of the strain rate in the

elastic modulus is detected. Only a slight reduction of the peak force can be seen as strain rate increases. The energy dissipation is smaller for higher strain rates. This can be associated to the fact that the conical and radial initiator dimensions are not optimized for this material; large longitudinal cracks are produced without maximizing the material degradation as in flat plate configuration. Figure 7: Force-displacement curves for different strain rates in 0/90 composite samples in flat plate configuration. Figure 8: Force-displacement curves for different strain rates in 0/90 composite samples with a conical initiator. Figure 9: Force-displacement curves for different strain rates in 0/90 composite samples with a conical initiator.

  • 4. Conclusions and future work

In this study different crashworthiness compressive tests have been proposed. The tests have been set up by tubular PVC samples. These tests allow measuring the crashworthiness of tubular structures subjected to different contour conditions. Three different initiator plugs have been proposed to carry out the compression tests: Flat, conical and radial ones and tests at different strain rates have been performed. Carbon-epoxy unidirectional and 0/90 composites have been tested under these conditions. For the selected initiators dimensions, no influence of the strain rate on the dissipative behaviour of compressed carbon-epoxy 0/90 tubes has been observed. As a future work to be done it is proposed to modify the geometry and dimensions of the initiator plugs to produce more severe conditions in the material, in order to reach and overcome the energy dissipated in flat plate configuration. Also a larger strain rate range will be studied to analyze its influence on the behaviour of composites under different initiator plugged compression tests. The final

  • bjective is to reach impact conditions in these tests.

Acknowledgments

The authors gratefully acknowledge the financial support for this research by the Basque Government within the scope of the Saiotek Program, Imdacomp1 project.

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5 CONCEPTION OF CRASH TESTS FOR COMPOSITE TUBULAR STRUCTURES

References

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