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Influence of Geometric Parameters of Conical Acrylic Portholes on Their Stress–Strain Behaviour

Abstract

Translucent elements in the form of truncated cones, which are made of organic glass, are widely used in the structures of portholes, submersible vessels, space vehicles, pressure chambers, teleboxes and other types of technical equipment. The decisive factor in designing portholes is to ensure the strength of their translucent elements. In order to reduce the weight of portholes and, accordingly, to increase the payload, it is necessary to optimise the geometric parameters of the translucent elements, which include the tapering angle and the ratio of thickness to radius of the smaller base. The paper deals with development of the applied (engineering) method for determining the stress–strain behaviour of the conical translucent elements of portholes made of organic glass under the action of a uniform hydrostatic pressure. Finite-element modelling of the translucent element of the conical porthole is performed, with the calculation of its stress–strain behaviour. External hydrostatic pressure of 10 MPa, absence of loads from the inside and continuous sliding of the translucent element with friction along the conical supporting surface of the porthole metal body are the boundary conditions for the computational model. Full-scale tests of translucent elements of portholes made of organic glass were performed under the action of uniform hydrostatic pressure. Analysis of the influence of geometric characteristics of the portholes on stress–strain behaviour showed that the increase in the tapering angle at the constant relative thickness of the translucent element reduced its axial displacement in all cases. Equivalent stresses acquire minimum values when the tapering angle is in the range from 75° to 105° (when the relative thickness increases, the optimal tapering angle becomes smaller). It is shown that the developed method for determination of the stress–strain behaviour of the conical translucent elements of portholes made of organic glass reflects the real picture of deformation and agrees with the results of full-scale tests. Results of the work allow us to choose the rational parameters of the translucent element for increasing the reliability of portholes through the creation of an effective distribution of stresses and strains in the translucent element, and improving its optical characteristics due to a relatively small deflection in operation.

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Influence of Geometric Parameters of Conical Acrylic Portholes on Their Stress–Strain Behaviour

Author: Kochanov, Vladimir; Píštěk, Václav; Kondratiev, Andrii; Yuresko, Tetyana; Kučera, Pavel
Publisher: MDPI
Year: 2022
DOI: 10.3390/polym14051041
Source: https://dspace.vut.cz/bitstreams/b0580978-8c33-42b5-8474-d2d03605afe3/download


Ci a ion: Kochano , V.; Píš ˇek, V.;
Kond a ie , A.; Yu esko, T.; Kuˇce a, P.
In luence o Geome ic Pa ame e s o
Conical Ac ylic Po holes on Thei
S ess–S ain Beha iou . Polyme s
2022,14, 1041. h ps://doi.o g/
10.3390/polym14051041
Academic Edi o : Beom Soo Kim
Recei ed: 15 Feb ua y 2022
Accep ed: 3 Ma ch 2022
Published: 5 Ma ch 2022
Publishe ’s No e: MDPI s ays neu al
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Copy igh : © 2022 by he au ho s.
Licensee MDPI, Basel, Swi ze land.
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A ibu ion (CC BY) license (h ps://
c ea i ecommons.o g/licenses/by/
4.0/).
polyme s
A icle
In luence o Geome ic Pa ame e s o Conical Ac ylic Po holes
on Thei S ess–S ain Beha iou
Vladimi Kochano 1, Václa Píš ˇek 2,* , And ii Kond a ie 3, Te yana Yu esko 1and Pa el Kuˇce a 2
1Depa men o Design and P oduc ion o S uc u es om Composi e Ma e ials, Admi al Maka o Na ional
Uni e si y o Shipbuilding, He oi Uk ainy A e. 9, 54025 Mykolayi , Uk aine; [email p o ec ed] (V.K.);
[email p o ec ed] (T.Y.)
2Ins i u e o Au omo i e Enginee ing, B no Uni e si y o Technology, Technická2896/2,
616 69 B no, Czech Republic; [email p o ec ed].cz
3
Depa men o Building Technology and Cons uc ion Ma e ials, O.M. Beke o Na ional Uni e si y o U ban
Economy in Kha ki , Ma shal Bazhano S . 17, 61002 Kha ki , Uk aine; [email p o ec ed]
*Co espondence: [email p o ec ed].cz; Tel.: +420-541-142-271
Abs ac :
T anslucen elemen s in he o m o unca ed cones, which a e made o o ganic glass, a e
widely used in he s uc u es o po holes, subme sible essels, space ehicles, p essu e chambe s,
eleboxes and o he ypes o echnical equipmen . The decisi e ac o in designing po holes is o
ensu e he s eng h o hei anslucen elemen s. In o de o educe he weigh o po holes and,
acco dingly, o inc ease he payload, i is necessa y o op imise he geome ic pa ame e s o he
anslucen elemen s, which include he ape ing angle and he a io o hickness o adius o he
smalle base. The pape deals wi h de elopmen o he applied (enginee ing) me hod o de e mining
he s ess–s ain beha iou o he conical anslucen elemen s o po holes made o o ganic glass
unde he ac ion o a uni o m hyd os a ic p essu e. Fini e-elemen modelling o he anslucen
elemen o he conical po hole is pe o med, wi h he calcula ion o i s s ess–s ain beha iou .
Ex e nal hyd os a ic p essu e o 10 MPa, absence o loads om he inside and con inuous sliding o
he anslucen elemen wi h ic ion along he conical suppo ing su ace o he po hole me al body
a e he bounda y condi ions o he compu a ional model. Full-scale es s o anslucen elemen s o
po holes made o o ganic glass we e pe o med unde he ac ion o uni o m hyd os a ic p essu e.
Analysis o he in luence o geome ic cha ac e is ics o he po holes on s ess–s ain beha iou
showed ha he inc ease in he ape ing angle a he cons an ela i e hickness o he anslucen
elemen educed i s axial displacemen in all cases. Equi alen s esses acqui e minimum alues
when he ape ing angle is in he ange om 75
◦
o 105
◦
(when he ela i e hickness inc eases, he
op imal ape ing angle becomes smalle ). I is shown ha he de eloped me hod o de e mina ion
o he s ess–s ain beha iou o he conical anslucen elemen s o po holes made o o ganic glass
e lec s he eal pic u e o de o ma ion and ag ees wi h he esul s o ull-scale es s. Resul s o
he wo k allow us o choose he a ional pa ame e s o he anslucen elemen o inc easing he
eliabili y o po holes h ough he c ea ion o an e ec i e dis ibu ion o s esses and s ains in he
anslucen elemen , and imp o ing i s op ical cha ac e is ics due o a ela i ely small de lec ion
in ope a ion.
Keywo ds: o ganic glass; polyme hyl me hac yla e plas ic; anslucen elemen ; hyd os a ic load
1. In oduc ion
The e a e a ious designs o po holes adop ed in cu en echnology, which can be
classi ied acco ding o he shape and ma e ial o he anslucen elemen [
1
,
2
]. Such di e si y
is a ibu ed o he di e ences in ope a ing condi ions o he po holes: wo king p essu e;
empe a u e and agg essi eness o he en i onmen ; load pa e n; image- egis a ion
me hod; and so on [
3
,
4
]. The anslucen elemen o he po hole as a pa o an op ical
sys em has a di ec e ec on image quali y, and i s s eng h p ede e mines he eliabili y
Polyme s 2022,14, 1041. h ps://doi.o g/10.3390/polym14051041 h ps://www.mdpi.com/jou nal/polyme s
Polyme s 2022,14, 1041 2 o 15
o he echnical equipmen as a whole [
5
–
7
]. The anslucen elemen is subjec o s ic
equi emen s on he c i e ia o s eng h, igh ness, de o ma ion o op ical su aces unde
load and op ical and he mophysical p ope ies o he ma e ial [8–10].
Conside ing he indica o s o s eng h, ailu e pa e n, manu ac u ing and p ocessing
echnology, i is mo e app op ia e o use he polyme hyl me hac yla e plas ic (PMMA o
o ganic glass o Ac ylic) as a ma e ial o anslucen elemen s [
11
]. The cha ac e is ics o
s eng h o anslucen elemen s made o PMMA ( he alue o p essu e a ailu e) depend
p ima ily on he a io o hickness h o diame e Do he po hole; and o conical and
sphe ical elemen s, on he ape ing angle αo he suppo ing su ace.
The mos undamen al ecommenda ions o he design and choice o he s uc u al
ype and geome ic pa ame e s o he ac ylic po holes o di e en s uc u al ypes a e
gi en in [
12
,
13
]. Pape [
14
] summa ises he in o ma ion abou s uc u al ypes o ac ylic
po holes bu does no gi e any algo i hms o selec ion o hei op imal shape depending
on ope a ing condi ions. Conside able a en ion in [
15
] is paid o he design o he po hole
body and ways o ensu e i s igh ness; howe e , no op imal enginee ing solu ions a e
p oposed. The au ho s o [
16
] ound ha a he ape ing angle o
α
= 90
◦
and ela i e
hickness o h/D= 0.41 no ensile s ains we e obse ed in he po hole, bu hey did no
assess he e ec o design pa ame e s on he po hole s ess s a e.
Calcula ion o he s ess–s ain beha iou o a anslucen elemen using classical
me hods o elas ici y heo y is e y ime-consuming in e ms o implemen a ion, since in
he p ocess o inding a solu ion, he mixed bounda y condi ions on h ee su aces ( wo
end su aces and a suppo ing conical su ace) should be ul illed [
17
]. Fu he mo e, i
is necessa y o conside he in luence o design pa ame e s, as well as he coe icien o
ic ion on he suppo [18].
Rega ding use o he bending heo y o hin pla es in he calcula ions o s ess–s ain
beha iou o he po holes, he e a e always signi ican e o s in he de e mina ion o
displacemen s wi h sligh ly ewe e o s han s ess de e mina ion. This is because ypical
dimensions o he po hole anslucen elemen ( hickness hand minimum diame e 2R
0
)
a e compa able, and he heo y o hin pla es can be applied a h/(R0≤1/5) [19,20].
Cu en ly, he s ess–s ain beha iou o anslucen elemen s is o en de e mined
using nume ical me hods [
21
]. The ini e-elemen me hod is he mos accu a e and uni e -
sal algo i hm o calcula ing he s ess–s ain beha iou o he class o s uc u es unde
s udy [
22
,
23
]. The me hods o calcula ion o conical po holes based on he ini e-elemen
me hod a e conside ed in [
24
–
26
]. I is shown ha he anslucen elemen unde he ac ion
o hyd os a ic p essu e slides wi h he ic ion o he conical suppo ing su ace o he
po hole body. A he same ime, he elas ic-plas ic s a e o he po hole made o ac ylic
glass is conside ed in [
24
], bu he c eeping a cyclic loads is no analysed. The au ho s
o [
25
] pe o med calcula ions o he po holes wi h h/D= 1,
α
= 90
◦
and coe icien o
ic ion on he suppo ing su ace = 0
−
0.2 unde he ac ion o p essu e P= 70 MPa,
which ag eed well wi h he esul s o expe imen s [
12
]. Howe e , he e is no da a on he
applicabili y o his calcula ion me hod o he po holes wi h h/D≤1.
Pape [
27
] shows ha he mos loaded elemen s o conical po holes a e he edges
o he low-p essu e su ace. Fo con i ma ion o he esul s, an expe imen al s udy was
conduc ed. A ew po holes we e manu ac u ed and es ed unde a hyd os a ic p essu e
o 60 MPa. Pape [
28
] deals wi h he de elopmen o a “design by analysis” me hod and
analysis o he s ess s a e o he po holes conside ing he c i e ia o ailu e o PMMA o
de e mine he p essu e and a ea o ailu e. The de ailed ini e-elemen model o he conical
po holes made o PMMA is de eloped in [
29
]. Based on his model, he s ess–s ain
beha iou o he po hole is analysed, and he causes o i s ailu e a e in es iga ed. The
esul s show ha local ailu e ends o occu a he co ne o he po hole cone whe e he
equi alen s esses acco ding o he Hube – on Mises s ain ene gy heo y a e maximal.
The expe imen al s udy o [
30
] shows he abili y o PMMA o “adap ” o he shape o
he po hole body. I was ound ha due o he plas ic beha iou o PMMA, he highes
mechanical s esses a dange ous poin s o he po hole a e educed by 64–71%. I con i med
Polyme s 2022,14, 1041 3 o 15
he easibili y o use o PMMA in he op ical sys ems’ echnology, bu he me hod o
de e mine i s eliabili y ac o is no speci ied in his pape .
The expe imen s and nume ical calcula ions o he s ess–s ain beha iou o PMMA
po holes a di e en le els o hyd os a ic p essu e o de elop a me hod o op imal design-
ing ega ding ope a ing condi ions a e desc ibed in [
31
]. Expe imen al dependences o
displacemen s o po holes made o PMMA a long- e m and cyclic impac s o hyd os a ic
p essu e a e ob ained.
Nume ical me hods a e known o hei e sa ili y, bu hey a e a he cumbe some
and di icul o apply in p ac ice [
32
,
33
]. A he same ime, explici solu ions o he
conical anslucen elemen s o he po holes made o PMMA unde he ac ion o uni o m
hyd os a ic p essu e a e limi ed by he necessi y o ul il he mixed bounda y condi ions and
ake in o conside a ion he in luence o s uc u al pa ame e s o a anslucen elemen and
coe icien o ic ion wi h he po hole body. These di icul ies, oge he wi h he limi ed
choice o undamen al unc ions om he ull ange o solu ions o he axisymme ic
p oblem o he elas ici y heo y, do no allow he bounda y condi ions o he anslucen
elemen o be ully me , while he mos s ess poin s a e always on he su ace o he
de o mable body. Howe e , based on hese me hods i is possible o ob ain ela i ely
simple bu ai ly accu a e applied solu ions o he p oblems [31,34].
Based on he analysis, he cu en ask is o de elop an applied (enginee ing) me hod
o he de e mina ion o he s ess–s ain beha iou o conical anslucen elemen s o he
po holes made o PMMA unde he ac ion o uni o m p essu e.
2. Ma e ials and Me hods
The conical anslucen elemen s o po holes made o PMMA a e s udied unde he
ac ion o uni o m p essu e. Classical me hods o elas ici y heo y (axisymme ic p oblem)
and he bending heo y o hick pla es a e used o de elop he applied (enginee ing) me hod
o he de e mina ion o he s ess–s ain beha iou o he conical anslucen elemen s. We
accep ed he ollowing hypo heses: In de o ma ion unde uni o m p essu e he anslucen
elemen bends and slides in he po hole body; he elemen mo es on he conical suppo ing
su ace wi h ic ion and wi hou sepa a ion om he su ace; he suppo eac ion on he
conical suppo ing su ace decomposes a each poin in o no mal and angen componen s.
To ind an analy ical solu ion, we used Lo e’s unc ion om polynomials o deg ees 3, 4 and
6, which we e ob ained using Legend e polynomials. Ful ilmen o he kinema ic and o ce
bounda y condi ions is achie ed by minimising he s anda d de ia ions o hese condi ions
along he gene a ing conical suppo ing su ace. Nume ical s udies we e conduc ed in he
so wa e package o he ini e-elemen analysis ANSYS Mechanical 2019 R1. In iew o
he axial symme y o he anslucen -elemen shape and ex e nal load, a na ow sec o
was used as a compu a ional model. The egula g id size was aken equal o 5 mm. Fo
he conical suppo ing su ace, a hal -sized g id was used, which allowed us o mo e
accu a ely model he anslucen elemen ’s in e ac ion wi h he me al ( i anium) body o
he po hole. Fo he ini e elemen o he po hole body, size o g id in he cen al zone
was aken equal o 10 mm; on he suppo ing su ace, whe e a sha p change in s ess could
be expec ed, 5 mm g id was used. The cons uc ed ini e-elemen model con ained mo e
han 10,000 Te a10 elemen s ( e ahed on wi h 10 nodes). Size o he g id was chosen
acco ding o dimensions o he eal po hole. S udy o he con e gence o he nume ical
solu ion showed ha wi h his numbe o ini e elemen s in he models he no mal and
shea s esses a ied sligh ly (by 5% a mos ). Analysis o he quali y o he cons uc ed
ini e-elemen models did no e eal any c i ical e o s. The p oblem o de e mina ion o
he po hole s ess–s ain beha iou was sol ed in he linea se ing. Full-scale es s we e
pe o med using he specialised expe imen al complex o hyd os a ic loads o anslucen
elemen s o he po holes. Tes s o po holes unde he ac ion o he hyd os a ic p essu e
we e pe o med in he high-p essu e chambe (chambe olume was 0.06 m
3
, maximum
p essu e was 150 MPa). Axial displacemen s we e measu ed by he mechanical dial gauge
ICh-10 (Mic o ech, Kyi , Uk aine) and elec ic-con ac manome e EKM-2U (UAM, Kyi ,
Polyme s 2022,14, 1041 4 o 15
Uk aine) was used o p essu e measu emen . P essu e in he chambe was c ea ed by he
pumping s a ion UNGR–2500R (UAM, Kyi , Uk aine). Specimens o anslucen elemen s
we e made o SO-120 PMMA (Admi al Maka o Na ional Uni e si y o Shipbuilding,
Mykolai , Uk aine) pla es o 50 mm hickness by u ning wi h subsequen polishing o he
op ical su aces.
3. Theo e ical Backg ound
Ma e ial o he anslucen elemen in he wo king posi ion is unde s a ic p essu e P
om he end su ace o high p essu e, as well as con ac (no mal and angen ial)-dis ibu ed
loads om he conical suppo ing su ace (Figu e 1).
Polyme s 2022, 14, x FOR PEER REVIEW 4 o 16
ac ion o he hyd os a ic p essu e we e pe o med in he high-p essu e chambe (chambe
olume was 0.06 m
3
, maximum p essu e was 150 MPa). Axial displacemen s we e meas-
u ed by he mechanical dial gauge ICh-10 (Mic o ech, Kyi , Uk aine) and elec ic-con ac
manome e EKM-2U (UAM, Kyi , Uk aine) was used o p essu e measu emen . P essu e
in he chambe was c ea ed by he pumping s a ion UNGR–2500R (UAM, Kyi , Uk aine).
Specimens o anslucen elemen s we e made o SO-120 PMMA (Admi al Maka o Na-
ional Uni e si y o Shipbuilding, Mykolai , Uk aine) pla es o 50 mm hickness by u n-
ing wi h subsequen polishing o he op ical su aces.
3. Theo e ical Backg ound
Ma e ial o he anslucen elemen in he wo king posi ion is unde s a ic p essu e P
om he end su ace o high p essu e, as well as con ac (no mal and angen ial)-dis ib-
u ed loads om he conical suppo ing su ace (Figu e 1).
Figu e 1. Po hole compu a ional model: P—hyd os a ic p essu e; —sliding wi h ic ion; 1— ans-
lucen elemen ; 2—po hole body.
The e a e no ex e nal loads on he end su ace o low p essu e. The e o e, bo h he
geome ic shape o he anslucen elemen and ex e nal su ace loads a e symme ic
a ound he cen al axis o he po hole, so he s ess–s ain beha iou o he anslucen
elemen is de e mined by sol ing he axisymme ic p oblem o he elas ici y heo y.
In case o he axisymme ic p oblem, nonze o componen s o he s ess–s ain beha -
iou in he cylind ical coo dina es can be exp essed in e ms o a biha monic Lo e’s unc-
ion [35–37] F( ,z):
𝑢=−1
2𝐺𝜕𝐹
𝜕𝑟𝜕𝑧;𝑤= 1
2𝐺󰇧2󰇛1−𝜇󰇜∇−𝜕
𝜕𝑧󰇨𝐹+𝑏
𝜎=𝜕
𝜕𝑧󰇧𝜇∇−𝜕
𝜕𝑟󰇨𝐹; 𝜎=𝜕
𝜕𝑧𝜇∇−1
𝑟𝜕
𝜕𝑟𝐹
𝜎=𝜕
𝜕𝑧󰇛2−𝜇󰇜∇−𝜕
𝜕𝑧𝐹; 𝜏 =𝜕
𝜕𝑟󰇛1−𝜇󰇜∇−𝜕
𝜕𝑧
(1)
whe e ∇=



+

+



is Laplace ope a o in he cylind ical coo dina es; u,w a e a-
dial and axial displacemen s, espec i ely; σ
, σ
θ
, σ
z
, τ
z
a e adial, angen ial, axial and
shea s esses; b
0
is ee cons an co esponding o he axial displacemen o he body.
Biha monic na u e o Lo e’s unc ion ensu es he exac ul ilmen o he equilib ium
equa ions


 +

 +
󰇛𝜎−𝜎󰇜=0;


 +

 +
𝜏 =0;
(2)
and equa ions o s ain compa ibili y

𝜎−𝜇󰇛𝜎−𝜎󰇜+
󰇛𝜎−𝜎󰇜=0; (3)
Figu e 1.
Po hole compu a ional model: P—hyd os a ic p essu e; —sliding wi h ic ion; 1—
anslucen elemen ; 2—po hole body.
The e a e no ex e nal loads on he end su ace o low p essu e. The e o e, bo h he
geome ic shape o he anslucen elemen and ex e nal su ace loads a e symme ic a ound
he cen al axis o he po hole, so he s ess–s ain beha iou o he anslucen elemen is
de e mined by sol ing he axisymme ic p oblem o he elas ici y heo y.
In case o he axisymme ic p oblem, nonze o componen s o he s ess–s ain be-
ha iou in he cylind ical coo dina es can be exp essed in e ms o a biha monic Lo e’s
unc ion [35–37]F( ,z):
u=−1
2G
∂2F
∂ ∂z;w=1
2G2(1−µ)∇2−∂2
∂z2F+b0
σ =∂
∂zµ∇2−∂2
∂ 2F;σθ=∂
∂zµ∇2−1
∂
∂ F
σz=∂
∂z(2−µ)∇2−∂2
∂z2F;τ z =∂
∂ (1−µ)∇2−∂2
∂z2
(1)
whe e
∇2=∂2
∂ 2+1
∂
∂ +∂2
∂z2
is Laplace ope a o in he cylind ical coo dina es; u,wa e
adial and axial displacemen s, espec i ely;
σ
,
σθ
,
σz
,
τ z
a e adial, angen ial, axial and
shea s esses; b0is ee cons an co esponding o he axial displacemen o he body.
Biha monic na u e o Lo e’s unc ion ensu es he exac ul ilmen o he equilib ium
equa ions
∂σ
∂ +∂τ z
∂z+1
(σ −σθ)=0;
∂τ z
∂ +∂σz
∂z+1
τ z =0;
(2)
and equa ions o s ain compa ibili y
∂
∂ σθ−µ(σ −σz)+1+µ
(σθ−σ )=0;
∂2
∂z2(σθ−µ(σ −σθ)) −2(1+µ)∂τ z
∂z+∂
∂ (σz−µ(σ +σθ)) =0.
(3)
Polyme s 2022,14, 1041 5 o 15
The e o e, solu ion o he p oblem o he axisymme ic s ess–s ain beha iou s a e o
he body o o a ion is educed o de e mina ion o Lo e’s s ess unc ion. Un o una ely, a
p esen he e is no analy ical ep esen a ion o Lo e’s unc ion sa is ying any p ede e mined
bounda y condi ions [35,36]. The explici solu ion o biha monic equa ion
∇2∇2F=0 (4)
is possible in he cylind ical coo dina es in in ini e se ies on he Bessel unc ions [
35
,
36
].
Howe e , his solu ion is incon enien o p ac ical use because o slow con e gence o
he se ies (o he o de 1
/√n
,n–se ial numbe o e ms o he se ies), pa icula ly unde
di icul bounda y condi ions and o noncylind ical bodies [
38
,
39
]. In addi ion, hey a e
inconsis en a he o igin o coo dina es a = 0.
The solu ion o Equa ion (4) in he sphe ical coo dina es in se ies using Legend e
polynomials wi h he u he ans o ma ion o he unc ion Fin o cylind ical coo dina es
is ela i ely simple; howe e , i is always necessa y o limi he numbe o e ms o se ies
in he expansion o he unc ion Fand sa is ac o y solu ions a e ob ained o he simple
bounda y condi ions only.
Ob aining dependences o he anslucen -elemen s ess–s ain beha iou , which can
be applied in p ac ice, in ol es a ce ain comp omise be ween accu acy and simplici y o
he solu ion. When cons uc ing an analy ical solu ion, i was necessa y o conside he
equi emen s below:
•
class o unc ions desc ibing he s ess–s ain beha iou o a anslucen elemen
should sa is y he biha monic Equa ion (4);
•
solu ion should ake in o accoun he in e ac ion o he anslucen elemen wi h eal
suppo , i.e., ensu e compliance wi h he bounda y condi ions he eon;
•
dependences o he componen s o he anslucen -elemen s ess–s ain beha iou
should be ela i ely simple.
S ess–s ain beha iou o he anslucen elemen depends on i s geome ic cha ac-
e is ics, which include he ape ing angle
α
and he a io o he smalle base diame e o
hickness Rmin/c(Figu e 2).
Polyme s 2022, 14, x FOR PEER REVIEW 5 o 16
𝑟



𝜎−𝜇󰇛𝜎−𝜎󰇜−2󰇛1+𝜇󰇜

 +
𝜎−𝜇󰇛𝜎+𝜎󰇜=0.
The e o e, solu ion o he p oblem o he axisymme ic s ess–s ain beha iou s a e
o he body o o a ion is educed o de e mina ion o Lo e’s s ess unc ion. Un o u-
na ely, a p esen he e is no analy ical ep esen a ion o Lo e’s unc ion sa is ying any
p ede e mined bounda y condi ions [35,36]. The explici solu ion o biha monic equa ion
∇∇𝐹=0 (4)
is possible in he cylind ical coo dina es in in ini e se ies on he Bessel unc ions [35,36].
Howe e , his solu ion is incon enien o p ac ical use because o slow con e gence o
he se ies (o he o de 1√𝑛
⁄, n–se ial numbe o e ms o he se ies), pa icula ly unde
di icul bounda y condi ions and o noncylind ical bodies [38,39]. In addi ion, hey a e
inconsis en a he o igin o coo dina es a = 0.
The solu ion o Equa ion (4) in he sphe ical coo dina es in se ies using Legend e
polynomials wi h he u he ans o ma ion o he unc ion F in o cylind ical coo dina es
is ela i ely simple; howe e , i is always necessa y o limi he numbe o e ms o se ies
in he expansion o he unc ion F and sa is ac o y solu ions a e ob ained o he simple
bounda y condi ions only.
Ob aining dependences o he anslucen -elemen s ess–s ain beha iou , which
can be applied in p ac ice, in ol es a ce ain comp omise be ween accu acy and simplici y
o he solu ion. When cons uc ing an analy ical solu ion, i was necessa y o conside he
equi emen s below:
• class o unc ions desc ibing he s ess–s ain beha iou o a anslucen elemen
should sa is y he biha monic Equa ion (4);
• solu ion should ake in o accoun he in e ac ion o he anslucen elemen wi h eal
suppo , i.e., ensu e compliance wi h he bounda y condi ions he eon;
• dependences o he componen s o he anslucen -elemen s ess–s ain beha iou
should be ela i ely simple.
S ess–s ain beha iou o he anslucen elemen depends on i s geome ic cha ac-
e is ics, which include he ape ing angle α and he a io o he smalle base diame e o
hickness R
min
⁄ c (Figu e 2).
Figu e 2. T anslucen -elemen loading diag am: h—hal - hickness o he anslucen elemen ; R
0
—
a e age adius.
When we choose he o igin o coo dina es in he cen e o he median su ace o he
anslucen elemen , bounda y condi ions a ends a e as ollows:
𝜎󰇡𝑟;−
󰇢=−𝑝; 𝜎󰇡𝑟;
󰇢=𝜏󰇡𝑟;
󰇢=0. (5)
Figu e 2.
T anslucen -elemen loading diag am: h—hal - hickness o he anslucen elemen ; R
0
—
a e age adius.
When we choose he o igin o coo dina es in he cen e o he median su ace o he
anslucen elemen , bounda y condi ions a ends a e as ollows:
σz ;−c
2=−p;σz ;c
2=τ z ;c
2=0. (5)

Polyme s 2022,14, 1041 6 o 15
In o de o ully de e mine he s ess–s ain beha iou o he anslucen elemen ,
we add he condi ions on he conical suppo ing su ace ad (Figu e 2) o he bounda y
condi ions (5)
Pτ= Pn, (6)
whe e is coe icien o ic ion.
The ollowing hypo heses a e in oduced:
•
in de o ma ion unde he uni o m p essu e P he anslucen elemen bends and slides
in he po hole body along he axis OZ;
•
he anslucen elemen mo es on he conical suppo ing su ace ad (i.e., a
=
R0− g α
2) wi h ic ion and wi hou sepa a ion om he su ace;
•
suppo eac ion P
on he conical suppo ing su ace ad decomposes in each poin
in o no mal Pnand angen ial Pτcomponen s.
Using he la e condi ion, i is possible o de e mine he ela ionship be ween he
adial P
and axial P
z
eac ions o he suppo ing su ace. Necessa y ope a ions o his
cons uc ion a e shown in Figu e 3.
Polyme s 2022, 14, x FOR PEER REVIEW 6 o 16
In o de o ully de e mine he s ess–s ain beha iou o he anslucen elemen , we
add he condi ions on he conical suppo ing su ace ad (Figu e 2) o he bounda y condi-
ions (5) 𝑃=
𝑓
𝑃, (6)
whe e is coe icien o ic ion.
The ollowing hypo heses a e in oduced:
• in de o ma ion unde he uni o m p essu e P he anslucen elemen bends and
slides in he po hole body along he axis OZ;
• he anslucen elemen mo es on he conical suppo ing su ace ad (i.e., a 𝑟=𝑅−
𝑡𝑔
) wi h ic ion and wi hou sepa a ion om he su ace;
• suppo eac ion P
on he conical suppo ing su ace ad decomposes in each poin
in o no mal P
n
and angen ial P
τ
componen s.
Using he la e condi ion, i is possible o de e mine he ela ionship be ween he
adial P
and axial P
z
eac ions o he suppo ing su ace. Necessa y ope a ions o his
cons uc ion a e shown in Figu e 3.
Figu e 3. Componen s o he ec o o suppo eac ions.
The e o e,
𝑃 =𝑃
𝑠𝑖𝑛
+𝑃𝑐𝑜𝑠
=𝑃
󰇡𝑠𝑖𝑛
+
𝑓
𝑐𝑜𝑠
󰇢;
𝑃 =𝑃
𝑐𝑜𝑠
−𝑃𝑠𝑖𝑛
=𝑃
󰇡𝑐𝑜𝑠
−
𝑓
𝑠𝑖𝑛
󰇢;
(7)
ha is,




=






. (8)
The anslucen -elemen suppo ing condi ions may be di e en , bu hey a e ul i-
ma ely educed o he o ce bounda y condi ions on he conical suppo ing su ace (i.e.,
he equilib ium equa ion o an elemen a y e ahed on) and a e w i en as:
𝜎𝑐𝑜𝑠
+𝜏𝑠𝑖𝑛
+𝑝 =0;
𝜎𝑠𝑖𝑛
+𝜏𝑐𝑜𝑠
+𝑝 =0; (9)
hence, we ob ain he ollowing ela ionship:




=













. (10)
A e Equa ions (8) and (10), he bounda y condi ion on he conical su ace o he
anslucen elemen is
Figu e 3. Componen s o he ec o o suppo eac ions.
The e o e,
P z =Pnsin α
2+Pτcosα
2=Pnsin α
2+ cos α
2;
P =Pncos α
2−Pτsin α
2=Pncosα
2− sin α
2;
(7)
ha is,
P z
P
= gα
2+
1− g α
2
. (8)
The anslucen -elemen suppo ing condi ions may be di e en , bu hey a e ul i-
ma ely educed o he o ce bounda y condi ions on he conical suppo ing su ace (i.e., he
equilib ium equa ion o an elemen a y e ahed on) and a e w i en as:
σ cos α
2+τ zsinα
2+p =0;
σzsin α
2+τ zcos α
2+p z =0;
(9)
hence, we ob ain he ollowing ela ionship:
p z
P
=σz gα
2+τ z
σ +τ z gα
2
. (10)
Polyme s 2022,14, 1041 7 o 15
A e Equa ions (8) and (10), he bounda y condi ion on he conical su ace o he
anslucen elemen is
σ +τ zβ−1− β
β+ (τ z +σzβ)=0, (11)
whe e β= g α
2.
Equa ion (11) is a condi ion o ic ion o he anslucen elemen on he conical
suppo ing su ace. The condi ion o con inuous sliding o he anslucen elemen is
w i en as
u+βw=0. (12)
Condi ions (5), (11) and (12) ully de e mine he su ace loads and displacemen s o
he anslucen elemen .
Pape s [
35
,
36
,
38
] show ha o exac co espondence o he bounda y condi ions (5)
on he end su aces o hick pla es, he deg ee o polynomials en e ing he unc ion in F
should no be highe han 6. To ind an analy ical solu ion, i is con enien o o m Lo e’s
unc ion o polynomials o deg ees 3, 4 and 6, ob ained wi h he use o he co esponding
Legend e polynomials [35,36]:
F=F3+F4+F6;
F3=a32z3−3 2z+b3 2z+z3;
F4=a48z4−24 2z2+3 4+b42z4+ 2z2− 4;
F6=1
3a616z6−120z4 2+90z2 4−5 6+b68z6−16z4 2−21z2 4+3 6;
(13)
whe e
a3
,
a4
,
a6
,
b3
,
b4and b6
a e a bi a y cons an s de e mined du ing ul ilmen o
bounda y condi ions.
Subs i u ion o (13) in (1) gi es he exp essions o s esses as shown below:
σz=−12a3+2(7−5µ)b3−192a4z+8(8−7µ)b4z+320a6−2z3+3 2z+
b664(7−11µ)z3−96(18 −11µ) 2z;
τ z =96a4 −4(8−7µ)b4z+240a64 z2− 3+
b6−96(7−11µ) z2+24(18 −11µ) 3.
(14)
Ful ilmen o bounda y condi ions o ype (5) a he ends a z=
±
callows us o
de e mine he a bi a y cons an s a3,a4,a6and b6:
a3=4(7−5µ)b3+p
24 ;a4=32(8−7µ)hb4−3p
768c;
a6=18 −11µ
40·704h3p;b6=p
4·704h3
(15)
A e subs i u ion o (15) in (13) we ob ain Lo e’s unc ion as
F=20(2−µ)b3+p
12 z3−20(1−µ)b3+p
8z 2+224(2−µ)hb4−3p
96hz4+224(1−µ)hb4−3p
32hz2 2−
224µhb4+3p
96h 4+p
256h38(3−µ)
15 z6−4(2−µ)z4 2+3(1−µ)z2 4+µ
6 6(16)
The co esponding unc ions (1) o he componen s o s ess–s ain beha iou o he
anslucen elemen a e w i en as ollows:
Polyme s 2022,14, 1041 8 o 15
2Gu =p
4 +5(1−µ)b3 +28(1−µ)b4−3p
8hz +p
32h34(2−µ)z3 −3(1−µ)z 3;
2Gw =b0−10b3µz−p
2z+3p
8hz2−14b42µz2+(1−µ) 2−3p
16h 2+p
128h3−8(1+µ)z4+24µz2 2+3(1−µ) 4;
σz=−p
2+pz
4h3−z2
h2;
τ z =3p
8hz2
h2−1;
σ =p
4+5b3(1+µ)+28(1+µ)b4z−3p
8hz+pz
32h34(2+µ)z2−3(3+µ) 2;
σθ=p
4+5b3(1+µ)+28(1+µ)b4z−3p
8hz+pz
32h34(2+µ)z2−3(1+3µ) 2.
(17)
Exp essions (17) show ha he coe icien b
3
de e mines he uni o m adial comp es-
sion, while b
4
is a pu e axisymme ic bending o he ound pla e. Coe icien b
0
co esponds
o he mo emen o he anslucen elemen as a solid objec in he po hole body along he
cen al axis z.
I is no possible o accu a ely implemen he o ce (11) and kinema ic (12) bounda y
condi ions. The e o e, we de ine a bi a y cons an s b
0
,b
3
and b
4
by minimisa ion o he
s anda d de ia ions o hese condi ions along he gene a ing conical suppo ing su ace.
The gene a ix equa ion in he accep ed coo dina e sys em (see Figu e 1) is gi en by:
=R0−zβ. (18)
Conside ing he mixed ( o ce and kinema ic) bounda y condi ions (11) and (12), we
can con enien ly p oceed o dimensionless exp essions o displacemen s and s esses (17).
To achie e his we in oduce new dimensionless a iables ζand ρ:
ζ=z
h;ρ=
R0
; (19)
and adop he no a ion
R0
h=γ. (20)
Conside ing (19) and (20), he gene a ix equa ion (18) is w i en as
ρ=1−βζ
γ. (21)
Subs i u ing (18) in o (17) and p oceeding o dimensionless coo dina es acco ding o
(19)
−
(21), we ob ain he exp essions o dimensionless displacemen s u,wand s esses
σz
,
σ ,σθand τ z on he conical suppo ing su ace a µ=1/3as below:
u=2Gu
ph =1
4(γ−βζ)+10
3(γ−βζ)b3+56(γ−βζ)ζb4−3
8(γ−βζ)ζ+5(γ−βζ)ζ3
24 −ζ(γ−βζ)3
16 ;
w=2Gw
ph =b0−10
3b3ζ−1
2ζ−28
3b4ζ2+3
8ζ2−28
3(γ−βζ)2b4−3
16(γ−βζ)2−1
12ζ4+1
16(γ−βζ)2ζ2+1
64(γ−βζ)4;
σz=σz
p=−1
2+3
4ζ−1
4ζ2;
τ z =τ z
p=3
8(γ−βζ)ζ2−1;
σ =σ
p=1
4+20
3b3+112
3b4−3
8ζ+7
24ζ3−5
16(γ−βζ)2ζ;
σθ=σ
p=1
4+20
3b3+112
3b4ζ−3
8ζ+7
24ζ3−3
16(γ−βζ)2ζ;
(22)
whe e b0=b0
pc ;b3=b3
p;b4=hb4
p.
A bi a y cons an
b3
is de e mined om he condi ion o s a ic equilib ium o he
anslucen elemen along he axis oz. The main ec o o hyd os a ic-p essu e o ces, P,
ac ing on he anslucen elemen , is balanced by he axial componen s P
z
o he conical
Polyme s 2022,14, 1041 9 o 15
suppo ing-su ace eac ions, which in u n a e co ela ed by ela ionship (8) wi h he eac-
ions o adial comp ession P
. Conside ing he equilib ium o one hal o he anslucen
elemen and es ablishing he dependence o he no mal s esses
σ
(p), being a e age on
diame ic c oss sec ion, and conside ing (22), we ob ain
b3=−3
80 (γ+β)2
λ!1− β
β+ +1. (23)
The emaining a bi a y cons an s a
0
and b
4
a e de e mined om he condi ion o
con inuous sliding o he anslucen elemen on he conical suppo ing su ace (12), and
a e w i en as:
Z1
−1(u+βw)2∂ζ →min. (24)
We de e mine he coe icien s b
0
,b
3
and b
4
om he condi ion o sa is ac ion o he
bounda y condi ions o sliding wi h ic ion on he conical suppo ing su ace a he
minimum dispe sion D. Wi h he use o he leas -squa es me hod in he in eg al o m, he
equa ion will be as ollows:
D=Z1
−1 (u−βw)2+σ +βτ z −1− β
+β(τ z +βσz)2!∂ζ →min. (25)
Thus, he unknown coe icien s a e de e mined om he sys em o equa ions:
∂D
∂b0
=0; ∂D
∂b3
=0; ∂D
∂b4
=0. (26)
4. Nume ical Implemen a ion
In iew o he axial symme y o he anslucen -elemen shape and ex e nal load, a
na ow sec o was used as a compu a ional model (Figu e 4a). I allowed us o educe
he numbe o ini e elemen s in he compu a ional model o he anslucen elemen ,
i.e., o educe he ime and o inc ease he accu acy o calcula ions wi h he same size o
he ini e-elemen g id as in he model as a whole. Since he e o o he ini e-elemen
me hod in de e mina ion o componen s o he s ess–s ain beha iou o s uc u es is o
o de 1
/n2
[
40
,
41
] (n–o de o di ision in o elemen s on one coo dina e), wi h a ull-size
anslucen -elemen hickness o 48 mm, he g id size was aken equal o 5 mm. Fo he
conical suppo ing su ace, a hal -sized g id was used; i allowed us o mo e accu a ely
model he anslucen elemen ’s in e ac ion wi h he me al ( i anium) body o he po hole.
Fo he ini e elemen o he po hole body, he size o g id in he cen al zone was aken
equal o 10 mm; on he suppo ing su ace, whe e a sha p change in s ess could be expec ed,
a 5 mm g id was used. The size o he g id was chosen acco ding o dimensions o he
eal po hole. The s udy o he con e gence o he nume ical solu ion showed ha wi h
his numbe o ini e elemen s in he models, he no mal and shea s esses a ied sligh ly
(by 5% a mos ). Analysis o he quali y o he cons uc ed ini e-elemen models did no
e eal any c i ical e o s. The p oblem o de e mina ion o he s ess–s ain beha iou o
he po hole was sol ed in he linea se ing.
As a esul , we ob ained he ollowing b eakdown o he po hole s uc u e in o ini e
elemen s (Figu e 4b).
Bounda y condi ions (5), (11) and (12) emained he same, bu since a model o he
na ow sec o o he anslucen elemen was used o he calcula ions by he ini e-elemen
me hod, bounda y condi ions o he F ic ionless Suppo ype we e se on ee-symme y
planes. This condi ion allowed us o ix he compu a ional model on he adial sec ions
o med by sepa a ion o a sec o om he ull-sized anslucen elemen wi hou ic ion
(i.e., a = 0) and wi h no no mal displacemen s o hese su aces. The F ic ionless Suppo
condi ion is used on he conical suppo ing su ace as well, a he coe icien s o ic ion