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Fracture predictions in impact three-point bending test of European beech

Abstract

Hardwood has become widespread in European forests. The strongest factor is climate change and damage to conifers by the bark beetle. The effort to study hardwoods grows with increasing volume of applications. Therefore, European beech wood was investigated under two impact loads in two material directions, resulting in four unique combinations supplemented by the measurement of the friction coefficient. Then, it was computationally simulated to reproduce the cracking, while the material model reflected the orthotropic behaviour in elasticity, plasticity and failure. The model was coded using the user subroutine in Abaqus to initiate and propagate the crack using the element deletion. The resulting reaction forces were in good agreement with those from the experiments. Cracking was numerically simulated in three of four cases as experimentally observed, however, upon larger deflections. Therefore, the model is applicable for further investigations.

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Fracture predictions in impact three-point bending test of European beech

Author: Kubík, Petr; Šebek, František; Hassan Vand, Mojtaba; Brabec, Martin; Tippner, Jan
Publisher: Springer Nature
Year: 2024
DOI: 10.1186/s10086-024-02157-x
Source: https://dspace.vut.cz/bitstreams/b1f2c109-ce7b-45c5-8397-7e778032074a/download
Kubíke al. Jou nal o Wood Science (2024) 70:42
h ps://doi.o g/10.1186/s10086-024-02157-x
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Jou nal o Wood Science
F ac u e p edic ions inimpac h ee-poin
bending es o Eu opean beech
Pe Kubík1, F an išek Šebek1* , Moj aba Hassan Vand2, Ma in B abec2 and Jan Tippne 2
Abs ac
Ha dwood has become widesp ead in Eu opean o es s. The s onges ac o is clima e change and damage o coni-
e s by he ba k bee le. The e o o s udy ha dwoods g ows wi h inc easing olume o applica ions. The e o e,
Eu opean beech wood was in es iga ed unde wo impac loads in wo ma e ial di ec ions, esul ing in ou unique
combina ions supplemen ed by he measu emen o he ic ion coe icien . Then, i was compu a ionally simu-
la ed o ep oduce he c acking, while he ma e ial model e lec ed he o ho opic beha iou in elas ici y, plas ici y
and ailu e. The model was coded using he use sub ou ine in Abaqus o ini ia e and p opaga e he c ack using
he elemen dele ion. The esul ing eac ion o ces we e in good ag eemen wi h hose om he expe imen s. C ack-
ing was nume ically simula ed in h ee o ou cases as expe imen ally obse ed, howe e , upon la ge de lec ions.
The e o e, he model is applicable o u he in es iga ions.
Keywo ds Aniso opy, Ba la , Dynamic, Explici , Flexu e, Rup u e
In oduc ion
Wood is a widesp ead na u al composi e, which has been
used as a cons uc ion ma e ial o cen u ies because i
is enewable, biologically deg adable, en i onmen ally
iendly, s ong, ligh weigh , easy o manu ac u e, elec i-
cally esis an , abso bing noise and aes he ic. The e o e,
models capable o p edic ing de o ma ion and ailu e
unde ope a ional o andom loading a e needed.
Bending is one o he common es s o wood. Jansson
[1] in es iga ed ailu e modes and s esses using s a ic
and impac bending es s showing dec easing impac
bending s eng h wi h dec easing ime o ailu e o he
Sp uce Pine Fi (SPF). Yoshiha a e al. [2] used a s a ic
h ee-poin bending es o de e mine he shea modulus
wi h he help o a co ec ion unc ion and a modi ied
Timoshenko beam o six wood species: Si ka sp uce,
wes e n hemlock, akama su, yellow popla , shioji and
balsa. Yoshiha a e al. [3] conduc ed a simila s udy o
asymme ic ou -poin bending es s. Yoshiha a and Oka
[4] ca ied ou he comp ession bending es o de e -
mine he elas ic modulus, p opo ional limi and bending
s eng h on specimens o Japanese i o a ious leng h-
o- hickness a ios. Then hey compa ed he esul s wi h
he con en ional bending es o con i m ha he co ec
lexu al p ope ies can be ob ained om he comp ession
bending es o a la ge leng h- o- hickness a io. Kubo-
jima e al. [5] used he impac bending es o es ima e
he elas ic modulus o Japanese ceda , hondo sp uce,
hiba a bo i ae, Japanese ed pine, paulownia, Manchu-
ian ash and Japanese e e g een oak. Polocoşe e al. [6]
in es iga ed he e ec o low- eloci y impac on ailu e
s esses and s i ness using he bending es consis ing o
a pendulum and specimens ha ing a leng h o 650mm,
wid h o 50mm and hicknesses o 20, 30 and 40mm
o ind ha ailu e was signi ican ly di e en compa ed
o quasi-s a ic es s o beech, la ch and pine. Polocoşe
e  al. [7] ound highe ene gy abso p ion in pine and
sp uce ein o ced wi h E-glass on he su ace loaded in
*Co espondence:
F an išek Šebek
[email p o ec ed].cz
1 Ins i u e o Solid Mechanics, Mecha onics and Biomechanics, Facul y
o Mechanical Enginee ing, B no Uni e si y o Technology, Technická
2896/2, 616 69 B no, Czech Republic
2 Depa men o Wood Science and Technology, Facul y o Fo es y
and Wood Technology, Mendel Uni e si y in B no, Zemědělská 810/3, 613
00 B no, Czech Republic
Page 2 o 12
Kubíke al. Jou nal o Wood Science (2024) 70:42
ension on a pendulum compa ed o specimens wi h-
ou ein o cemen . The ac o was 1.4 o pine and 2.5
o sp uce. Jacques e al. [8] ca ied ou ull-scale es ing
on indi idual ligh ame lumbe s made om SPF. Then,
he ou -poin bending es s wi h s ain a es o 6 × 10–6
o 4 × 10–1 s–1 se ed o p opose he s ess–s ain ela-
ionship applicable o he modelling o blas loadings.
Olmedo e al. [9] ollowed he dynamic esponse o esh
s ems unde impac loading using he Mou on–Cha py
pendulum. Then hey analysed he load-bea ing capac-
i y o wooden cons uc ions made o elled ees se ing
as p o ec ion agains alling ocks. B anche iau e al. [10]
p oposed an analy ical ela ionship, which con e s he
elas ic modulus es ima ed om he h ee-poin bend-
ing es o he elas ic modulus appea ing in he ou -
poin bending es . The esul s we e expe imen ally
alida ed on specimens om six wood species wi h di -
e en densi ies. Di e en elas ic moduli o sp uce and
oak in h ee- and ou -poin bending es s we e also
analysed by Babiak e al. [11]. Ga e al. [12] examined
he e ec o he mal modi ica ion o Eu opean oak and
No way sp uce using he Cha py pendulum o ind ha
changes in basic chemical componen s and impac bend-
ing s eng h we e less a ec ed o oak han o sp uce.
The e ec o he mal modi ica ion on impac bend-
ing s eng h was also in es iga ed by Hassan Vand and
Tippne [13] o ind ha he mal modi ica ion caused a
dec ease in de lec ion and maximum longi udinal s ain
up o app oxima ely 50% acco ding o digi al image co -
ela ion (DIC) o h ee-poin bending es s o i e wood
species: ash, beech, la ch, oak and sp uce. Hassan Vand
e al. [14] also es ed he e ec o mois u e con en on
he beha iou o h ee wood species o beech, oak and
sp uce. They e alua ed he wo k equi ed o ini ia e he
c ack and b eak he specimens and ound, using DIC,
ha he maximum de lec ion and longi udinal ensile
s ain inc eased wi h inc easing mois u e con en .
The minimum o he li e a u e deals wi h he compu-
a ional modelling o wood unde impac . The e o e, his
wo k ocuses on he dynamic beha iou o Eu opean
beech (Fagus syl a ica L.) unde he h ee-poin bend-
ing es . All es s we e ca ied ou using a d op-weigh
impac es ing machine wi h wo hamme s o achie e
a ious impac eloci ies. Then, nume ical simula ions
ollowed o de elop a ma e ial model wi h good ac-
u e p edic abili y compa ed o expe imen s. I should
be no ed ha many wo ks [15, 16] use he o ho opic
yield c i e ion acco ding o Hill [17] o he desc ip ion
o plas ic beha iou . Howe e , some ma e ial pa ame e s
( h ee ou o six) o he equi alen s ess can be nega i e
due o signi ican ly dis inc yield s esses in espec i e
wood di ec ions [18–20]. The nega i e ma e ial pa ame-
e s can hen cause he equi alen s ess o be unde ined.
The e o e, he o ho opic yield c i e ion acco ding o
Ba la e al. [21] will be used o o e come his issue.
Expe imen s
Ma e ial
The ma e ial s udied was Eu opean beech belonging o
ha dwoods. The specimens we e made om ee g own
nea B no (Czech Republic). The wood was conside ed
o ho opic wi h a di ec ion pa allel wi h h ee p ima y
(heigh ) g ow h called longi udinal (L), a di ec ion pe -
pendicula o he ee p ima y g ow h passing h ough
he pi h o he ee called adial (R) and a di ec ion pe -
pendicula o ee g ow h and simul aneously as a an-
gen o annual ings called angen ial (T) as depic ed in
Fig.1. All specimens we e s o ed in a clima ic chambe a
a empe a u e o 20°C and a ela i e humidi y o 65% o
p oduce a uni o m equilib ium mois u e con en o 12%.
Th ee‑poin impac bending es
All specimens we e manu ac u ed wi h ib es o ien ed
along he leng h o 300mm ha ing a squa e c oss sec-
ion wi h an edge o 20mm. Be o e es ing, specimens
we e weighed in analy ical balance wi h 1mg eadabil-
i y, which esul ed in an a i hme ic mean o densi y o
727kg/m3 wi h a s anda d de ia ion o 33kg/m3. The
symme ic h ee-poin bending was ca ied ou in wo
ma e ial di ec ions R and T (Fig. 1), espec i ely. The
span- o-dep h a io was 12, esul ing in a suppo span o
240mm. Bo h he suppo s and he hamme had a adius
o 15mm and a su ace oughness Ra o 0.2μm.
The es s we e pe o med on he d op-weigh impac
es ing machine DPFes 400 om Labo ech ( igh Fig.2)
a oom empe a u e. Two di e en hamme s we e
d opped om wo ini ial heigh s o ob ain wo impac
eloci ies as gi en in Table1 o p o ide a di e se ma e ial
o nume ical simula ions. The es ing machine au oma -
ically measu ed he ue impac eloci ies (Table1). Fo
each o hese wo condi ions, 6 specimens we e es ed in
he R and T di ec ions, esul ing in 4 da ase s. The ham-
me displacemen was measu ed wi h 0.01 mm p eci-
sion, while he o ce was measu ed using a piezoelec ic
o ce ansduce CFT + 50 kN om HBM a ached o he
hamme .
The es s we e eco ded wi h Fas cam SA-X2 om
Pho on. The high-speed came a had a cell size o 20μm
and was equipped wi h a Nikon Mic o-Nikko G lens
wi h a ocal leng h o 105mm and a Nikon Z TC-2.0 × .
I was placed app oxima ely 0.9m om he la e al speci-
men su ace, which was pa allel o he came a senso .
Addi ional ligh ing was ensu ed by wo Mul iLed QT
s andalone lamps (le Fig.2). The ield o iew was i -
ed o a cen al pa o la e al specimen’s su ace wi h a
hamme . Images wi h a esolu ion o 1024 × 672px we e
Page 3 o 12
Kubíke al. Jou nal o Wood Science (2024) 70:42
cap u ed wi h a ame a e o 20,000 ps. The image pos -
p ocessing was pe o med in Vic-2D 2010 so wa e om
Co ela ed Solu ions. In o de o de e mine he con-
e sion ac o , a simple calib a ion was done using he
one-dimensional scale de ined by he known dis ance.
The displacemen ield was calcula ed om he ield o
3 × 3p . The Lag ange s ain ield was de e mined wi h
he lowes possible s ain il e size o 5 × 5p so ha he
maximum possible spa ial esolu ion was achie ed. In
20
T
LR
L
R
T
20
240
300
R15
R15
R15
Fig. 1 Loading in he R ( op) and T di ec ions (bo om) wi h all ma e ial di ec ions du ing impac h ee-poin bending es s (all dimensions in mm)
Impac es
i
ng mac
hi
n
e
H
igh
-spee
d
came a
L
ED
ligh
s
D
a a ac
q
u
i
s
i
i
on s
y
s e
m
Fig. 2 High-speed came a wi h accesso ies (le ) and d op-weigh impac es ing machine ( igh )
Page 4 o 12
Kubíke al. Jou nal o Wood Science (2024) 70:42
addi ion, he op ical measu emen se ed o he analysis
o he ac u e (i any).
Measu emen o  ic ion coe icien
T ibological expe imen s we e pe o med o collec inpu
o nume ical modelling. The es s we e ca ied ou using
he Uni e sal Mechanical Tes e (UMT) T iboLab om
B uke (Fig.3). The pin o 5mm in diame e was made
o AISI 52100 alloy s eel ha ing a su ace oughness Ra
o 0.2μm, he same as he suppo s and he hamme in
he h ee-poin impac bending es . I was o ced agains
wooden specimens by 196 N, which was measu ed by a
dual o ce senso DFH-100 wi h a sampling equency
o 100 Hz and co esponded o a con ac p essu e o
10MPa. This con ac p essu e was chosen as i eached
ens o MPa in he ollowing nume ical simula ions. The
pin oscilla ed wi h a equency o 2Hz and ampli ude
o 5mm o 120s. Six specimens wi h dimensions o
40 × 20 × 10mm we e es ed. These specimens we e man-
u ac u ed om he same ee as hose o he h ee-poin
impac bending es and s o ed in he clima ic chambe
o each he same uni o m equilib ium mois u e con en
o 12%. The pin was o ced agains h ee LR and h ee LT
su aces o 40 × 20mm mo ing in he R and L di ec ions,
espec i ely. The e o e, he measu emen was wi hin
one annual ing o he L di ec ion and app oxima ely 5
annual ings o he R di ec ion wi h an a e age annual
ing wid h o 2.5mm.
The pin ajec o y was 10mm, bu he esul s we e p o-
cessed in MATLAB R2024a o a 6-mm-long po ion o
he specimen in o de o omi he dead ends whe e he
pin decele a ed and accele a ed. Then, he conside ed
ic ion was kine ic and a ea o e alua ion app oxima ely
50 mm2. Also, he e alua ion was no conduc ed o he
beginnings o he es s whe e a ploughing was p esen .
Nume ical simula ions
The calcula ions we e pe o med in Abaqus/Explici
comme cial code based on he explici o mula ion o he
ini e elemen me hod. The ma e ial model was imple-
men ed using he VUMAT use sub ou ine, as i is no
a s anda d one. The ailu e was modelled by dele ing ele-
men s ha eached c i ical damage, which is a simple
echnique ha does no equi e emeshing, con a y o
he node sepa a ion me hod.
Model o ma e ial
The hamme and suppo s we e made o s eel, which is
much s i e han he es ed wood specimens. The e o e,
he s eel pa s we e modelled as igid, sa ing some com-
pu a ional ime. On he con a y, wood was modelled
as a homogeneous o ho opic con inuum. The he e o-
genei y was neglec ed o sa e some compu a ional ime
again h ough ma e ial model simpli ica ion, including i s
calib a ion.
The o ho opic elas ici y was desc ibed by he gene al-
ised Hooke’s law as
whe e
εi
,
Ei
and
σi
a e he no mal s ain, elas ic modulus
and no mal s ess, espec i ely,
εij
,
νij
,
Gij
and
σij
a e he
enso ial shea s ain, Poisson’s a io, shea modulus and
shea s ess o
i,j=L,R,T
, espec i ely. All elas ic con-
s an s (Table2) we e aken om [20], whe e he disin e-
g a ion o he same wood was ca ied ou unde a ious
s ain a es in a ious ma e ial di ec ions.
The o ho opic plas ici y was desc ibed by he model
o Ba la e al. [21], who p oposed he yield condi ion as
(1)







εL
εR
εT
εLR
εRT
εTL







=










1
EL
−
νLR
EL
−
νLT
EL
000
−
νRL
ER
1
ER
−
νRT
ER
000
−
νTL
ET
−
νTR
ET
1
ET
000
0001
2GLR
00
0 0 001
2GRT
0
0 0 0001
2G
TL

















σL
σR
σT
σLR
σRT
σTL







(2)
σB−σy=0,
Table 1 Con igu a ion o he impac h ee-poin bending es s
Hamme
weigh
(kg)
Ini ial
heigh
(mm)
A e age ue
impac eloci y
(m/s)
Numbe o
specimens
(–)
Ma e ial
di ec ion
(–)
9.05 458.87 2.70 6 R
9.05 458.87 2.70 6 T
4.55 815.77 3.25 6 R
4.55 815.77 3.25 6 T
D i in
g
mechanism
Sp
ec
i
men
h
o
ld
e
Sp
ecimen
Pin
F
o
ce
se
n
so
L
oa
di
n
g
mec
h
an
i
sm
Fig. 3 UMT T iboLab used o measu emen o ic ion coe icien
Page 5 o 12
Kubíke al. Jou nal o Wood Science (2024) 70:42
whe e
σy
is he yield s ess, which is dependen on he
equi alen plas ic s ain (Fig.4), while
σB
is he equi a-
len s ess acco ding o Ba la e al. [21] as
(3)
σ
B
=1
m
√2
m
|
K1
−
K2
|
m
+|
K2
−
K3
|
m
+|
K3
−
K2
|
m
,
whe e
m
is he exponen (in luencing he shape o he
yield su ace),
K1,K2
and
K3
a e he p incipal alues o
he linea ly ans o med de ia o ic s ess enso
whe e
a
,
b
,
c
,
,
g
, and
h
a e he ma e ial pa ame e s,
which we e i ed (Table3; Fig.5) so ha he yield su ace
co esponded o ha in [20], whe e he model o Hill [17]
was used wi h a nega i e ma e ial pa ame e
(H<0)
. A
change in he yield c i e ion was sough due o he elimi-
na ion o a nega i e ma e ial pa ame e esul ing om a
signi ican di e ence in he yield s esses in he L di ec-
ion compa ed o o he s (R and T in Fig.5), which can
be p oblema ic in some cases. The yield c i e ion was
aken om [20], whe e i was no necessa y o model di -
e en yield s esses in ension and comp ession in ini e
elemen s. Then, he yield c i e ion was ecalib a ed o
Eu opean beech, s ill neglec ing he s eng h di e en ial
e ec . Howe e , mo e sophis ica ed yield c i e ia should
be conside ed when signi ican di e ences in ensile and
comp essi e yield s esses we e obse ed.
(4)
K
=



c
(σL
−
σR)
−b
(σT
−
σL)
3hσLR gσTL
hσLR a(σR−σT)−c(σL−σR)
3 σRT
gσTL σRT b(σT−σL)−a(σR−σT)
3


,
Table 2 Elas ic cons an s o Eu opean beech wood [20]
Ma e ial di ec ion L R T LR RT TL
Elas ic modulus (MPa) 13,000 3500 3000 – – –
Poisson’s a io (–) – – – 0.302 0.362 0.318
Shea modulus (MPa) – – – 1608 460 1059
00.2 0.4 0.6 0.8 1.0
Equi alen plas ic s ain [–]
0
10
20
30
40
50
Y
i
e
ld
s ess [MPa]
Fig. 4 Flow cu e o he Eu opean beech wood [20]
Table 3 Plas ici y- ela ed ma e ial pa ame e s o Eu opean beech
m
(–)
a
(–)
b
(–)
c
(–)
(–)
g
(–)
h
(–)
2 2.357 0.862 0.009 0.456 0.642 0.525
15
30
37.5
22.5
7.5
–7.5
–22.5
–37.5
–75 –45 –15 15 45 75 –75
–45
–15
15
45
75
R[MPa]
2
3
(
(
0,5
T[MPa]
2
3
(
(
0,5
R[MPa]
L[MPa]
2
3
(
(
0,5
L
[MPa
]
LR [MPa]
Fig. 5 Yield locus in he Haigh–Wes e gaa d space (le ) and he space o wo no mal and one shea s esses ( igh ) o he Eu opean beech wood

Page 6 o 12
Kubíke al. Jou nal o Wood Science (2024) 70:42
The o ho opic cumula i e damage was desc ibed by
he damage pa ame e as:
whe e
ε
i
,
εD
i
and
εp
i
a e he ac u e s ain, plas ic s ain
o a gi en loading pa h and plas ic s ain, espec i ely.
As men ioned abo e, he elemen is emo ed when he
c i ical alue is eached, speci ically when
max (Di)=1
.
Fu he mo e, ac u e s ains a e dependen on s ess
iaxiali y (apa om he a e dependence in oduced
la e ) o inco po a e he ension/comp ession ailu e
asymme y (which is simple han he ac u e models in
[15, 22–24])
whe e
σm
is he mean s ess
and
σ
is he equi alen s ess acco ding o on Mises
The dependence o ac u e s ains on s ess iaxial-
i y was based on [20] and was u he e ined using he
ial and e o me hod using ens o nume ical simula-
ions so ha he esul s ma ched expe imen al obse a-
ion in impac h ee-poin bending es s. F ac u e s ains
dependen on he s ess iaxiali y,
ε
i
(η
)
, a e shown in
Fig.6 o he e e ence equi alen plas ic s ain a e o
1 s–1.
Finally, ac u e s ains we e addi ionally depend-
en on he equi alen plas ic s ain a e as expe imen s
we e conduc ed a a ious impac eloci ies. Con a y
o he linea a e dependence in [20] o signi ican ly
g ea e s ain a es, an exponen ial dependence on he
equi alen plas ic s ain a e based on he equa ion p o-
posed by Johnson and Cook [25] was ecalib a ed o i
he expe imen s as ollows (using
ε
i
(η
)
ha has al eady
been calib a ed p e iously o he e e ence equi alen
plas ic s ain a e o 1 s–1)
whe e
C
is he ma e ial pa ame e , calib a ed as 0.1 a e
se e al addi ional nume ical simula ions o e e ence
(5)
D
i=
ε
D
i

0
1
ε
i

dεp
i
,
(6)
η=
σm
σ
,
(7)
σ
m
=
σ
L
+σ
R
+σ
T
3,
(8)
σ=
1
√2
(σL
−
σR)2
+
(σR
−
σT)2
+
(σT
−
σL)2
+
6σ2
LR
+
6σ2
RT
+
6σ2
TL
.
(9)
ε
i=ε
i(η)

1+Cln

˙
ε
p
˙
ε0
,
equi alen plas ic s ain a e
˙
ε
0=1s
−1
. Finally,
˙
εp
is he
equi alen plas ic s ain a e
whe e
˙εp
is he plas ic s ain a e enso .
Model o geome y andbounda y condi ions
As men ioned abo e, he ad an age o he elemen dele-
ion echnique is i s simple implemen a ion. Howe e ,
i has i s d awbacks as i depends on he size o he ele-
men , which is usually kep as small as possible o eal-
is ically p opaga e he c ack using one o wo elemen s.
The e o e, he elemen s had a size o 0.1mm in a eas o
wood ailu e as well as in con ac egions (Fig.7). O he
a eas we e meshed wi h elemen s o a size o 1.82mm.
Only a 0.1-mm-wid h specimen was modelled as a plane
s ain o ep esen he inne laye o wood ins ead o
using 20mm o sa e conside able compu a ional ime.
Geome y was meshed wi h 8-node linea b ick ini e
elemen s wi h educed in eg a ion and hou glass con-
ol (labelled C3D8R in Abaqus). The mesh consis ed o
128,774 nodes and 63,850 elemen s o which 4 we e addi-
ionally 6-node linea wedge ini e elemen s wi h educed
in eg a ion and hou glass con ol (labelled C3D6R in
Abaqus) nea he con ac egions whe e he ine mesh
changed in o coa se mesh (highligh ed in ed in Fig.7).
As men ioned ea lie , he hamme and suppo s we e
modelled as igid, he e o e, as su aces which come
in o con ac wi h he specimen. The wid h o he igid
(10)
˙
ε
p
=
2
3˙
εp
:˙
εp
,
S ess iaxiali y [–]
–0.5 00.5 1.0
0
0.5
1.0
1.5
2.0
F ac u e s a
i
n [–]
0
L
R
T
Fig. 6 F ac u e s ain o all ma e ial di ec ions and he e e ence
equi alen plas ic s ain a e o 1 s–1
Page 7 o 12
Kubíke al. Jou nal o Wood Science (2024) 70:42
bodies, 0.3mm, was g ea e han he wid h o he spec-
imen, 0.1mm, and we e cen ed wi h each o he . The
hamme and suppo s we e meshed wi h 4-node bilin-
ea quad ila e al igid ini e elemen s (labelled R3D4
in Abaqus) ha ing a size o 0.1mm, he e o e, 3 ele-
men s pe wid h. One suppo , modelled he same as
a hamme , had 1892 nodes and 1416 elemen s. Mo eo-
e , an elemen was added o he e e ence poin o he
hamme (highligh ed by a blue pen ag am in Fig.7) in
o de o inco po a e he olume load (labelled MASS
in Abaqus), equi alen o he hamme weigh .
Displacemen s and o a ions o e e ence poin s o
he suppo s we e es ic ed. The same applies o he
hamme excep o he e ical displacemen . The
ini ial eloci y was p esc ibed in his di ec ion, co -
esponding o he a e age ue impac eloci y o he
expe imen (Table1). The specimen had cons ained
displacemen s only in he wid h di ec ion o simula e
he plane s ain condi ion ( he geome y o he speci-
men was disc e ised by 1 elemen along he wid h).
The accele a ion due o g a i y o 9.807 m/s2 was
applied on he whole geome y in he di ec ion o
impac .
In addi ion o he de ini ion o he con ac be ween
he specimen, hamme and suppo s, sel -con ac was
applied o all elemen edges in he a ea o expec ed
ailu e (whe e he elemen s wi h 0.1mm edges we e).
I ensu ed he con ac o new ee su aces, which we e
no ini ially p esen in he geome y, eme ging a e
he elemen dele ion ha simula ed he c acking. The
no mal beha iou o he con ac s was se as ‘ha d’ o
allow any p essu e when he su aces a e in con ac ,
while he ic ion coe icien o 0.15 ob ained om he
expe imen s in he p e ious sec ion was se in he an-
gen ial di ec ion.
Resul s anddiscussion
Figu es8 and 9 summa ise all he o ce esponses agains
he hamme displacemen s ob ained om he impac
es ing machine o hamme s ha weighed 9.05 and
4.55kg, espec i ely. The DIC did no se e o ob ain
he displacemen s. The do ed lines highligh he es s in
which he specimens emained in ac . The co espond-
ing specimens bended o wa d and back ( he hamme
e u ned app oxima ely o he e e ence posi ion co e-
sponding o he displacemen o 0mm—i is ze o de lec-
ion). The dashed-do ed lines highligh he es s in which
he specimens pa ially b oke (did no b eak h ough he
whole heigh ). The co esponding specimens exhibi ed
signi ican sp ingback, he e o e, he hamme e u ned
app oxima ely o he e e ence posi ion. The solid lines
highligh he es s in which he specimens ailed (b oke
h ough he en i e heigh ). The co esponding specimens
emained ben a e he es (all in Fig.8). Mo eo e , he
momen o c ack ini ia ion is highligh ed by a ci cle. The
a e age alue o he hamme displacemen co espond-
ing o he momen o c ack ini ia ion is highligh ed by a
hick e ical dashed g ey line. This line is no plo ed in
le Fig.9, whe e only 2 ou o 6 specimens pa ially b oke
and none ailed o he hamme weighing 4.55kg loading
in he R di ec ion. Only 1 specimen ailed o he ham-
me ha weighed 4.55kg in he T di ec ion ( igh Fig.9).
O he specimens pa ially b oke, while he specimen co -
esponding o Tes 6 in igh Fig.9 was c acked along
almos he whole heigh unde hese condi ions, he e-
o e, he hamme s a ed e u ning la e .
The a i hme ic mean ic ion coe icien o 0.15 wi h
a s anda d de ia ion o 0.005 was measu ed i espec-
i e o he ma e ial di ec ion. Then, he expe imen ally
and compu a ionally ob ained esul s a e compa ed
in Figs.10 and 11. The p edic ed o ces we e in good
Fig. 7 Fini e elemen mesh wi h de ails
Page 8 o 12
Kubíke al. Jou nal o Wood Science (2024) 70:42
ag eemen wi h he expe imen s be o e he maximum
de lec ion. Fo ces oscilla ed mo e in nume ical simula-
ions han in impac h ee-poin bending es s. Howe e ,
his is an in insic ea u e o explici dynamics. C ack-
ing was p edic ed la e in nume ical simula ion han in
expe imen s o a 9.05kg hamme in Fig.10. No c acking
0246810 12 14
Displacemen [mm]
0
1000
2000
3000
4000
Fo ce [N]
Tes 1
Tes 2
Tes 3
Tes 4
Tes 5
Tes 6
0246810 12 14
Displacemen [mm]
0
1000
2000
3000
4000
Fo ce [N]
Tes 1
Tes 2
Tes 3
Tes 4
Tes 5
Tes 6
R, 9.05 kg T, 9.05 kg
Fig. 8 Fo ce–displacemen esponses o a 9.05 kg hamme in he R (le ) and T di ec ions ( igh ), espec i ely ( o in e p e a ion o he e e ences
o colou in his igu e legend, he eade is e e ed o he web e sion o his a icle)
0246810 12 14
Dis
p
lacemen [mm]
0
1000
2000
3000
4000
Fo ce [N]
T, 4.55 kg Tes 1
Tes 2
Tes 3
Tes 4
Tes 5
Tes 6
0246810 12 14
Dis
p
lacemen [mm]
0
1000
2000
3000
4000
Fo ce [N]
R, 4.55 kg Tes 1
Tes 2
Tes 3
Tes 4
Tes 5
Tes 6
Fig. 9 Fo ce–displacemen esponses o a 4.55 kg hamme in he R (le ) and T di ec ions ( igh ), espec i ely ( o in e p e a ion o he e e ences
o colou in his igu e legend, he eade is e e ed o he web e sion o his a icle)
0246810 12 14
Dis
p
lacemen [mm]
0
1000
2000
3000
4000
Fo ce [N]
R, 9.05 kg Expe imen s
Simula ion
0246810 12 14
Dis
p
lacemen [mm]
0
1000
2000
3000
4000
Fo ce [N]
T, 9.05 kg Expe imen s
Simula ion
Fig. 10 Compa ison o o ce–displacemen esponses om nume ical simula ions and expe imen s o a 9.05 kg hamme in he R (le ) and T ( igh )
di ec ions, espec i ely
Page 9 o 12
Kubíke al. Jou nal o Wood Science (2024) 70:42
was achie ed o he R di ec ion wi h a 4.55kg hamme
(le Fig. 9) compu a ionally o ep oduce he expe i-
men s (le Fig.11). Howe e , pa ial c acking was no
achie ed compu a ionally o he T di ec ion wi h a
4.55kg hamme as in he expe imen s ( igh Fig.9). The
elas ic s ain ene gy was so high in nume ical simula ions
o ha case ha led o he p edic ion o c ack p opa-
ga ion along he whole heigh , con a y o he impac
h ee-poin bending es s whe e specimens b oke jus
pa ially ( igh Fig. 9). The homogenei y o he model
also con ibu ed o he lack o p edic ion o c ack a es ,
which occu ed in expe imen s a e some delamina ion
because, among o he s, he wood is s ongly inhomoge-
neous. This should be aken in o accoun by modelling
he geome y based on da a om compu ed omog aphy
speci ically o each specimen, which migh no be p ac-
ical o indus ial applica ions.
The p edic ed con ou s o he damage pa ame e a e
displayed in Figs.12 and 13 a e he impac h ee-poin
bending es s compa ed o expe imen s app oxima ely
in scale. Howe e , i should be no ed ha he p edic ed
de lec ions a e g ea e (app oxima ely 1.5mm), as is e i-
den om Figs.10 and 11. The damage pa ame e s
DR
and
DT
eached hei c i ical alue in espec i e R and T
0246810 12 14
Dis
p
lacemen [mm]
0
1000
2000
3000
4000
Fo ce [N]
R, 4.55 kg Expe imen s
Simula ion
0246810 12 14
Dis
p
lacemen [mm]
0
1000
2000
3000
4000
Fo ce [N]
T, 4.55 kg Expe imen s
Simula ion
Fig. 11 Compa ison o o ce–displacemen esponses om nume ical simula ions and expe imen s o a 4.55 kg hamme in he R (le ) and T ( igh )
di ec ions, espec i ely
R, 9.05 kg T, 9.05 kg
38.029.000.185.076.057.033.024.005.080.071.052.00.00
Fig. 12 Expe imen s ( op) compa ed o p edic ed con ou s o he damage pa ame e (bo om) o he 9.05 kg hamme and he R (le ) and T ( igh )
di ec ions (app oxima ely in scale)