Finite Element Analysis of the O-ring Behavior Under Uniform
Squeeze Levels and Internal Pressure
E.EL BAHLOUL1, H. AISSAOUI1, M. DIANY 2, E. BOUDAIA 2, S. TOUAIRI2
1Automation and Energy Conversion Team, Faculty of Science and Technology, Sultan Moulay Sliman University, Beni
Mellal, MOROCCO
2Industrial Engineering Laboratory, Faculty of Science and Technology, Sultan Moulay Sliman University, Beni Mellal,
MOROCCO
Abstract: - The variety of applications, in all industrial fields, whether for routine use or a specific application, requires
the design of increasingly efficient sealing systems. O-rings are fundamental elements in many industrial devices and
machines, thanks to advantages such as low cost, small size, cleanliness, and ease of assembly. Moreover, the O-ring is
available in thousands of dimensions.
In this work, the analysis of the mechanical and leakage behavior of the O-ring seal, when installed either in a groove or
between two plates, is presented.
The behavior of the assemblies in both scenarios when the clamping force and fluid pressure are applied is investigated
using two numerical models generated with Ansys software.
The numerical model findings are compared to the analytical approach based on Hertz contact theory and other
researchers' experimental results. This study shows that the use of a groove to ensure the mounting of elastomeric O-rings
is important in pressurized installations. Furthermore, for different pressure conditions, the reliability of the O-ring
strongly depends on three parameters: compression ratio of the seal, the hardness of the seal, and the friction coefficient.
Keywords: - O-ring, groove, analytical model, finite element model, contact pressure, fluid pressure
Received: December 23, 2021. Revised: November 6, 2022. Accepted: December 4, 2022. Published: December 31, 2022.
1. Introduction
The modern industry nowadays handles a lot of polluting,
toxic, radiative, and flammable products which require
more precise knowledge of the sealing function to avoid any
possible leakage of these dangerous products. In practice,
commercial O-rings are designed to increase contact
pressure as the fluid pressure increases. They also require a
secure seal, as well as economical manufacturing and easy
assembly. Due to its symmetrical shape and inexpensive
production cost, the O-ring may appear to be an easy-to-use
and effective seal at first glance.
When consulting patent databases, it is only in the 1930s
that the term "O-ring" appears. The O-ring was invented by
Niels Christensen to seal a piston/cylinder application [1].
Lindley [2] points out the lack of scientific results that
would allow a better understanding of the functioning of O-
rings. And indeed, research on O-rings did not begin until a
few years after these. The equations developed until today
to analytically determine the distribution of the contact
pressure against the joint-structure contact surfaces are
deduced from the classical Hertzian contact theory [3]. Less
attention was paid to O-rings inserted in grooves until 1988
when Dragoni et al. [4] studied the mechanical behavior of
a non-pressurized O-ring installed in a rectangular groove.
The seal in this study is modeled by a flat disk and is
subjected to an axial deformation due to the clamping force.
This concept was subjected to numerical, experimental, and
analytical analysis. Karaszkiewicz [5] has just completed
and enriched these previous models, with an analytical
model allowing determining the geometrical distortion, the
width, and the contact pressure of an O-ring subjected to
radial compression and installed in a rectangular groove.
This model enables for the fluid pressure exerted to the
joint to be taken into account. The numerical results of
George [6] have supported the findings of this study.
However, the equations proposed in this model have an
error of up to 30% which explains the difficulty of modeling
the mechanical behavior of O-rings in pressurized
installations. Eshel [7] uses an experimental setup to predict
the fluid pressures that cause O-ring extrusion to determine
the parameters of his analytical model. Also, as a function
of service pressures and the hardness of the rubber utilized,
establish the limitations of mechanical extrusion clearance.
In 1998, Yokoyama et al. [8] experimentally determined the
change in contact pressure as a function of change in fluid
pressure for an O-ring installed in an axial assembly. The
seals used were Polyacrylate (ACM), Fluorocarbon (FKM)
propylene (EPDM) with different hardnesses. The results
obtained show that the lower the hardness of the seal, the
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higher the rate of change of the contact pressure at the seal-
structure contact surfaces as a function of the fluid pressure.
Other experimental works [9], [10], [11] have obtained a
satisfactory agreement with the theoretical results. They
proposed a photoelasticity-inspired test method. They
devised the method to investigate the contact pressure
distribution and internal stresses of an O-ring in a
rectangular groove. Other researchers [12], [13] will focus
on the effect of the friction coefficient on O-ring sealing
performance.
In assemblies with O-rings, finite element analysis is present
in the majority of published works. This approach has been
used on a variety of seals in the literature, including
rectangular seals [14], [15], U-shaped seals [16], [17], and
O-rings [18], [19]. Using the same method Diany et al. [20]
[21] developed a finite element model to study the short-
term relaxation of a non-pressurized O-ring. This study
showed the effect of the groove in reducing the initial crush
required to create the contact pressure that can ensure
sealing. El Bahloul et al. [22] have shown that one of the
main parameters in the evaluation of O-rings installed in a
groove is undoubtedly the contact pressure distribution
between the seal and the contact surfaces and that the
proper functioning of the O-ring depends on the best choice
of the values of the extrusion clearance and the coefficient
of friction in pressurized installations. In other works [23],
[24], the same authors studied the effect of the groove shape
and the effect of introducing a metal core inside the
elastomer O-ring. The results of the first study showed that
the use of a concave groove, or rectangular groove link,
produces more contact pressure and thus further limits the
risk of leakage. The second study showed that the
introduction of a metal core inside the elastomeric O-ring
can improve not only the strength of the seal but also the
maximum value of the contact pressure.
O-rings are fundamental elements in many industrial
devices and machines, thanks to advantages such as low
cost, small size, cleanliness, and ease of assembly. In
addition, the O-ring is available in thousands of sizes.
However, seal failure due to incorrect mounting conditions,
wrong choice of O-ring material, or O-ring geometry leads
to lower system performance. Conversely, a better
knowledge of the characteristics of the O-ring and its
support will improve the performance and efficiency of the
systems being sealed. It will prolong the seal's life, allowing
it to be employed in a variety of industrial applications. In
this work, finite element models, using Ansys software [25],
are proposed to evaluate the behavior of the O-ring
assembly subjected to combined loads: clamping force and
fluid pressure.
2. Modeling of the Studied Assemblies
Large elastic deformations and quasi-incompressible
behavior are required when modeling the mechanical
behavior of elastomers. Thus, mechanical behavior laws
must be formulated in the context of large deformation
modeling [26],[27],[28]. The behavior laws most commonly
used by commercial calculation software are Mooney
Rivlin, Ogden, and Neo Hook. The so-called hyperelastic
model of Mooney Rivlin [29] is the most commonly
encountered model for describing the mechanical behavior
of elastomers. This one allows describing correctly the
behavior of an elastomer up to a strain level of 200 % [30].
Knowing all the geometrical parameters as well as the
behavior law of the seal material, the positioning of the O-
ring can be simulated. The elements of the assembly are
simulated in their operating position taking into account the
geometrical conditions of the ISO 3601 standard [31].
Figure 1 shows the studied assemblies. Table I lists the
mechanical and geometrical features of the assemblies. The
joint is modeled by a disk with 2D planar elements with
four nodes (PLANE182). Contact elements, CONTA171
and TARGE169, are used to simulate the reaction between
the elements that are in contact. Figure 2 shows an example
of the O-ring mesh.
d0
Figure 1 - O-ring assembly between two plates (Assembly
1), O-ring assembly in a groove (Assembly 2)
Table I - Mechanical and geometrical characteristics of the
assemblies
Symbol
Contact
B1
O-ring -
groove
B2
B3
A1
O-ring-
plates
A2
Values
0
d
16.35 mm
2
d
2.65 mm
1
E
13.8 MPa
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Figure 2 - O-ring meshes
The simulation of the joint assemblies was performed in two
steps. In the first step, the joint is compressed between a
plate and a groove (Figure 3 (b)) or between two plates
(Figure 4 (b)) under the assumption of large deformations
and large displacements. The plates and grooves were
defined as rigid analytical elements. The displacements of
the inner plate in assembly 1 and the groove in assembly 2
were canceled in all directions. The top plate in both
assemblies, whose displacements are canceled in the radial
direction, is axially loaded by a uniformly distributed
clamping force. In the second step, fluid pressure is applied
to the active side of the joint (Figure 3 (c) and Figure 4 (c))
for all surface elements that are not in contact with the
groove and plates.
Figure 3 - (a) Mounting the O-ring in a groove. (b)
Compression of the O-ring. (c) Application of fluid pressure
Figure 4 - (a) Mounting the O-ring between two plates. (b)
Compression of the O-ring. (c) Application of fluid pressure
3. Conventional Analytical Theory
This part summarizes the set of equations that give the
distribution of the contact pressure, the maximum value of
this contact pressure, and the length of the contact that
characterizes the joint-plate contact area. The joint-plate
contact has been treated by Lindley [2] by adapting the
classical theory of Hertz. This researcher developed a
simple equation that expresses the compressive load, F, as a
function of the compression ratio of the joint, C, according
to the equation.
3
*6
2
02 (1.25 50 )F d d E C C

(1)
The compression ratio of the joint, C, is determined as a
function of the crushing values, e, and the diameter of the
joint cross-section
2
d
. It is expressed as follows:
2
C e d
The contact width,
l
, the maximum value of contact
pressure,
0
P
are given by equations (2) and (3).
*
*
4
2PR
lE
(2)
02
0
4F
pdl
(3)
With
*
R
the relative radius of curvature and
*
E
the
equivalent modulus of elasticity.
The relative radius of curvature,
*
R
, is determined
according to the type of contact. Thus in the case of the
plane-cylinder contact adopted by Lindley we have
*2
2
d
R
(4)
The equivalent modulus of elasticity is given by equation
(5).
*1
2
1
1
E
E
(5)
The distribution of the contact pressure as a function of the
radial position on the joint is given by equation (6).
2
0
2
( ) 1 x
p x p l




(6)
4. Results and Discussions
To verify the finite element models developed in this
chapter, we have made comparisons with the theoretical
results presented by Lindley [2] and the experimental results
of Kim et al. [32]. A first simulation is performed
Geometry of PLANE182
2D elements with four
nodes (I, J, K, L)
O-ring
Meshing of the O-
ring cross section
with PLANE182 2D
elements
Groove
Top plate
O-ring
Fluid pressure
Contact surfaces
(a)
(b)
(c)
Top plate
Lower plate
O-ring
Contact surfaces
Fluid pressure
(a)
(b)
(c)
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considering a zero fluid pressure and a zero friction
coefficient. results were obtained with the FE model
presented in Figure 4 and compared to the results of the
values of equation (1) developed by Lindley [2] and those
published by Kim et al. [32]. We note a very good
agreement between the results obtained by the analytical
model and the results of the FE model. However, there is a
significant discrepancy between the two models and the
experimental test of Kim et al. for compression ratios
greater than 15%. This difference may be due to the
geometrical and physical data considered by the authors
when establishing their model.
Both the analytical and numerical models are used to
determine the contact width values and contact pressure
distribution profiles when a clamping load is applied. Figure
6 shows a comparison between the contact width values
given by equation (2) and the FE model results shown in
Figure 4. The FE model results are the average value of the
last nodes in contact and the first nodes not in contact. The
difference between the numerical and analytical curves is at
most 5% at a clamping force of 350 N, which corresponds
to a compression ratio of 27% in this case. It is important to
recall that Lindley [2] describes the relationship of contact-
displacement force, contact width, and contact pressure as a
function of O-ring radial position for a maximum O-ring
compression ratio of 25%.
Figure 7 shows the contact pressure distributions on the
surface A1 defined in Figure 1 for four values of clamping
force. This figure also shows a comparison between the
analytical and numerical models. The contact pressure
profiles have a parabolic shape that confirms the Hertzian
shape. The comparison between the values of the analytical
model and the results of the FE analysis indicates that the
maximum contact pressure increases as the clamping force
increases and the difference between the two models do not
exceed 4%. From these remarks, we can confirm that there
is a good agreement between the two approaches, analytical
and FE, when the only load applied is the clamping force.
The effect of friction was considered from the finite element
simulation of assemblies 1 and 2 shown in Figures 3 and 4.
The axial and radial deformations of the O-ring as a
function of clamping force and fluid pressure are obtained
for
f
values of 0, 0.1, and 0.2 (Figure 8). This figure
shows the importance of the location of this type of seal in
a groove. For a clamping force of 700 N and a fluid
pressure of 0.75 MPa, the increase in the friction
coefficient considerably reduces the axial and radial
deformation of the seal. Indeed, for friction coefficients
0, 0.1 and 0.2. The elongation decreases respectively
from 66.5, 19.5 to 2.7%. Regarding the compression ratio,
it decreases respectively from 48.9, 37.3 to 30.9. In
conclusion, the deformation of the joint as a function of
the clamping load and the pressure of the fluid depends
strongly on the value of the friction coefficient.
Figure 9 shows the variation of the maximum
contact pressure, at the surfaces B1, B2 and B3 defined in
Figure 3, for two values of friction coefficients 0.05
and 0.2,
according to the pressure of the confined fluid. It can be
seen that the influence of the friction coefficient on the
contact pressure is negligible. Furthermore, by studying
Figure 10, the increase of the friction coefficient can
decrease the maximum value of the von Mises stress inside
the O-ring installed in a groove for high fluid pressures and
the opposite for low fluid pressures.
Given the particularity of the material characteristics of the
O-ring, a parametric study to understand the influence of
Young's modulus E becomes necessary. Several simulations
were performed, for the same geometry of the FE model
presented in Figure 3, for Young's modulus ranging
from 6.96 MPa to 17.3 MPa. The numerical calculations
were carried out with a coefficient of friction of 0.2.
Figure 11 shows the evolution of the compression ratio
C, obtained for three values of Young's modulus E,
weighting the two phases of deformation of the seal:
clamping phase F, and pressurization phase P. The results
delivered by this figure serve as a basis for determining the
influence of these three parameters on the compression
ratio of the seal in the throat. It is obvious that the
compression ratio increases with increased clamping force
and decreases with increasing fluid pressure. As can be
seen in the same figure, the compression ratio is
proportional to Young's modulus. It can be observed in
the clamping phase that, the stiffer the seal material, the
lower the compression ratio will be. On the other hand,
when the fluid pressure is applied and increases
further, the value of the compression ratio decreases.
It is also observed that the curves corresponding to the
three values of Young's modulus are inverted when the
fluid pressure exceeds 4.75 MPa.
Figure 12 shows the contact pressure distribution curves at
the contact surfaces B1, B2 and B3 defined in Figure 1, for
a compression ratio of 20% and a fluid pressure of 5 MPa.
The simulations are performed for several values of E. The
curves in this figure confirm that the stresses are
proportional to the moduli of elasticity for the same
deformation. Thus, when the joint stiffness is greater, the
contact pressure is greater. Figure 13 shows the variation of
the maximum value of Von Mises stress inside the seal for
three values of E as a function of fluid pressure for a
compression ratio of 20%. Regardless of the value of E, the
maximum Von Mises stress increases with increasing rates
as the fluid pressure increases. We note that the difference
between the three seal hardnesses shows a high value for
pressures below 5.5 MPa and remains relatively low for
fluid pressures above this value. This result does not
surprise us. Indeed, whatever the value of E, when the fluid
pressure is applied and its value increases, the zone where
the stress is maximum moves towards the outside of the
joint to the side of the extrusion gap. Lastly, it is worth
mentioning that the compression ratio as a function of
clamping force - Numerical/ analytical/ experimental
comparison is presented in Figure 5.
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Figure 5 - Compression ratio as a function of clamping
force - Numerical/ analytical/ experimental comparison
Figure 6 - Contact width versus clamping force -
numerical/analytical comparison
Figure 7 - Distribution of contact pressure as a function of
clamping force - numerical/analytical comparison
Figure 8 - The influence of the friction coefficient on the
deformation of the O-ring
Figure 9 - The influence of the friction coefficient on the
maximum contact pressure
0.05f
0.2f
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Figure 10 - The influence of the friction coefficient on the
maximum value of the Von Mises stress
Figure 11 - Variation of compression ratio with the
variation of clamping force and fluid pressure
Figure 12 - Influence of Young's modulus on the contact
pressure distribution for a compression ratio of 20% and a
fluid pressure of 5 MPa
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Figure 13 - influence of Young's modulus on the maximum
value of the Von Mises stress for a compression ratio of
20%
5. Conclusions
This work is devoted to the study of the mechanical and
leakage behavior of pressurized assemblies equipped with
an O-ring which is placed in a groove and between two
plates. The material behavior of the O-ring has been
described by the Mooney Rivlin behavior law. The finite
element model of the gasket was carried out with
axisymmetric elements under the assumption of large
displacements and large deformations using the commercial
software (ANSYS).
The combined effect of clamping load and fluid pressure
has been analyzed for both assemblies. The numerical
results obtained are compared with the experimental results
published by Kim et al. [20] and theoretically based on the
classical Hertz theory. The comparison is made only on the
clamping force, contact width, and contact pressure. They
show agreement and confirm the classical form of the
contact pressure distribution.
This study shows that the use of a groove to ensure the
assembly of elastomer O-rings is important in pressurized
installations. On the other hand, under the same loading
conditions, the reliability of the O-ring is strongly
dependent on three parameters: compression ratio of the O-
ring, its hardness, and the friction coefficient.
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Contribution of Individual Authors to the
Creation of a Scientific Article (Ghostwriting
Policy)
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