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Abaqus Technology Brief
                                                                                                                  TB-09-PEN-1
                                                                                                             Revised: July 2009


Earth Penetration Simulation using Coupled Eulerian-Lagrangian Analysis


Summary
In earth penetration events the projectile generally strikes
the target at an oblique angle. As a result, the projectile is
subjected to a multi-axial force and acceleration history
through impact. The effectiveness of an earth penetration
system is enhanced by the ability to withstand severe
lateral loading. Consequently, it is important to under-
stand how such loads develop during an impact event.
In this Technology Brief, Abaqus/Explicit is used to simu-
late the impact of a high-strength steel penetrator into a
concrete target. The penetrator/target interaction is ana-
lyzed using the coupled Eulerian-Lagrangian methodol-
ogy. Specifically, the penetrator is modeled in a tradi-
tional Lagrangian framework while the concrete target is
modeled in an Eulerian framework. It will be shown that
Abaqus/Explicit results are in good agreement with pub-
lished experimental data.                                                                Click to animate

Background                                                          Key Abaqus Features and Benefits
The in-service accelerations that an earth-penetrating
projectile experience can depend on the obliqueness of               Coupled Eulerian-Lagrangian capability allows the
impact. As the impact condition deviates from the limiting             general contact interaction of Eulerian and La-
case of being perfectly normal to a flat surface, the accel-           grangian regions of a model, simplifying the simu-
erations lateral to the projectile’s body axis increase.               lation of the extreme deformation associated with
                                                                       impact events
It is well known that such ‘non-normal’ impact conditions
produce large lateral forces and accelerations that can              Concrete damaged plasticity model simulates
threaten the survivability of the penetrator case and inter-           damage due to complex stress states
nal components [1]. Clearly, a predictive capability that
allows for simulation of an oblique impact penetration               Accelerometer connector elements measure ac-
event provides the means to better design earth penetrat-              celerations in a body-fixed coordinate system
ing systems.
                                                                     Anti-aliasing run-time filters simplify the removal
A high-speed impact event very often involves extreme                  of noise from results
states of deformation and/or material failure. A traditional
Lagrangian finite element approach, in which elements            tor impacting concrete. As outlined in [1], a series of ex-
deform as the associated material deforms, is limited in         periments was undertaken in which concrete test targets
the extent of deformation an element can sustain. An Eul-        were subjected to penetrator impacts at different angles
erian formulation differs however, in that material flows        of obliquity. The recorded acceleration results will be
through a mesh of nodes that remain fixed in space; the          compared to those of an Abaqus/Explicit analysis, in
Eulerian framework is thus ideally suited for analyses that      which the penetrator is modeled with Lagrangian ele-
involve extreme levels of deformation, up to and including       ments and the concrete is modeled as an Eulerian mate-
material failure and rupture. Abaqus/Explicit allows full        rial.
coupling of Lagrangian elements and Eulerian material
domains in an analysis through simple general contact            Analysis Approach
definitions.
                                                                 The penetration test under consideration is illustrated in
This Technology Brief considers the coupled Eulerian-            Figure 1. The concrete target is of a cylindrical shape
Lagrangian (CEL) analysis of high-strength steel penetra-        and is cast in a thin-walled steel pipe. It is cut to an angle
2

                                                                The objective is to create a mesh that is adequately re-
                                                                fined near the contact zone while keeping the total num-
                                                                ber of elements to a minimum. To achieve this goal, the
                                                                mesh resolution is biased in such a way that the mesh
                                                                becomes coarser away from the contact zone. A mesh
                                                                refinement study was conducted, and a uniform grid spac-
                                                                ing of 5 mm in the immediate area of impact was found
                                                                satisfactory. This 5 mm grid extends out uniformly in both
                                                                in-plane directions for about 5 projectile diameters, be-
                                                                yond which the grid is graded out to the boundaries. In
                                                                the direction of penetration, a uniform mesh with a 5 mm
                                                                resolution is used. The final Eulerian mesh consists of
                                                                approximately 1 million elements. The duration of the dy-
                                                                namic analysis is 7 milliseconds.

Figure 1: Cross-sectional schematic view of test configu-       To measure acceleration, an accelerometer-type connec-
                         ration                                 tor element is placed at the center of the acceleration re-
                                                                cording device (shown in Figure 2). This type of connector
of 30 degrees with the cylinder axis.                           provides a convenient way to measure acceleration in a
                                                                coordinate system fixed to a moving body.
Figure 2 shows the cross section of the projectile used in
the test. Its case is made of 4130 steel.  During the test, a   Material Models
smooth-bore powder gun launched the projectile with a
striking velocity of 334 m/s.   The direction of the impact     The concrete damaged plasticity model is used to capture
velocity was aligned with the axis of the cylinder such that    the constitutive behavior of the concrete. With the inclu-
the angles of pitch and yaw (i.e. the amount of misalign-       sion of multi-hardening plasticity and isotropic damaged
ment between the velocity and projectile axes) were both        elasticity, the model is ideal for applications where con-
less than one degree and could be safely neglected.             crete is subject to monotonic, cyclic or dynamic loading.

The projectile’s acceleration was measured with a forward       It assumes that the two main failure mechanisms are ten-
mounted accelerometer that collected data at                    sile cracking and compressive crushing. For this analysis,
10μs intervals. The data was filtered with a two-pass, four-    the associated data were derived from hydrostatic and
pole Butterworth filter with a cutoff frequency of 2 kHz.       shear failure envelopes given in [1]. While not included in
                                                                this analysis, the effect of strain-rate dependence can be
Finite Element Model                                            added for an even higher level of fidelity.
The full three-dimensional projectile is modeled with ap-       The penetrator case, steel pipe, and penetrator internal
proximately 13,000 Lagrangian hexahedral reduced-               components are modeled with linear elastic materials.
integration elements. The target is modeled with an Eule-       This is based on the assumption that the amount of abra-
rian mesh, including both the concrete and the thin-walled      sion and erosion of the penetrator nose is small and the
steel pipe. The Eulerian mesh is extended beyond the
initial volume of concrete so that fragments created during
impact are accounted for. A cross section of the assem-
bled model is shown in Figure 3.




                                                                Figure 3: Cross section of assembled coupled Eulerian-
        Figure 2: Cross-sectional view of projectile                              Lagrangian model
3

penetrator wall does not yield. The material properties for
the internal components were chosen such that the cor-
rect penetrator weight and moments of inertia were
achieved.
Contact Interactions and Loadings
The interaction between the Eulerian target and Lagran-
gian penetrator is handled through the general contact
capability in Abaqus/Explicit, which automatically detects
and resolves contact interactions.

Results
The primary quantities of interest from the test are the
axial and lateral projectile accelerations, the depth of
penetration, and the rest (turning) angle.  
                                                                Figure 5: Depth of penetration and rest (turning) angle
Acceleration histories
                                                               direction (Figure 2). This makes the axial deceleration of
The time history plot of both the axial (blue) and lateral     the projectile positive. The lateral acceleration direction is
(green) accelerations is shown in Figure 4. Both the test      aligned with the negative global Y direction.
(dashed) and the simulation (solid) results are shown.
Good correlation is observed between the test and simu-        The axial acceleration profile in Figure 4 shows that from
lation results, with peak acceleration difference less than    initial impact until the penetrator nose is buried, the decel-
5%.                                                            eration  increases. After that, the deceleration decreases
                                                               in the general trend of the experimental data.
Simulation of high-speed impact events with explicit finite
element schemes is known to produce noisy results. Anti-       Initiated by asymmetric loads (due to the oblique impact)
aliasing filters are provided in Abaqus (during run time in    during nose burial, the penetrator pitches upward and
the solver phase or in the post-processing phase) to con-      eventually the tail impacts the side of the hole created by
veniently filter the noise. The acceleration data shown in     the burrowing penetrator. The bending of the beam-like
Figures 4 and 6 have been filtered using a sine-               penetrator body due to the large inertial loading immedi-
Butterworth filter with a cutoff frequency of 2 kHz.           ately after the initial impact exacerbates this “slap-down”
                                                               process. The effect from this significant short-duration
To be consistent with the experimental setup, the axial        lateral loading is evident in the lateral acceleration profile
acceleration direction is aligned with the negative global X   in Figure 4. As the event progresses, secondary lateral
                                                               loads continue to produce peaks in the profile as the
                                                               penetrator body contacts the sides of the hole.
                                                               Depth of Penetration
                                                               Results for the final depth of penetration and the rest
                                                               (turning) angle are shown in Figure 5 and Table 1. As with
                                                               the acceleration results, there is good correlation between
                                                               the test and the simulation. Figure 6 contains an animation
                                                               that provides a synchronized view of the penetration defor-
                                                               mation and the acceleration time history. Note that the peak
                                                               von Mises stress shown is well below the yield strength of
                                                               1345 MPa for the 4130 steel penetrator case, except in
                                                               the region near the nose where localized erosion is ex-
                                                               pected and was actually observed during the test.

                                                                              Nose Tip    Nose Tip      Path        X'‐Y'
                                                                                 X'          Y'        Length    Rest Angle
                                                                                (m)         (m)          (m)     (degrees)
                                                               Test            0.62        0.69         0.93        43.0
                                                               FEA             0.60        0.80         1.00        36.9
Figure 4: Comparison of Abaqus/Explicit and measured           Table 1: Path length and rest angle results and measure-
acceleration histories. Note that deceleration is positive.                             ments
4




  Figure 6: Synchronized animation of deformation, acceleration time histories, and von Mises stress in penetrator case.
                                                    Click to animate

Summary
                                                                                                    approach correlate very well with the chosen experimen-
A coupled Eulerian-Lagrangian finite element based ap-                                              tal data and demonstrate the utility of the coupled ap-
proach to the simulation of earth penetration events is                                             proach to modeling high-speed impact events that involve
demonstrated using Abaqus/Explicit. The results from this                                           material damage and extreme levels of deformation.



References
1. Stokes, E., Yarrington, P. and Glenn, L., “An Earth Penetration Modeling Assessment: Prediction of Lateral Loading
   for Oblique Impact Conditions”, UCRL-TR-213206, Lawrence Livermore National Laboratory,
   Livermore, California, 2005. https://e-reports-ext.llnl.gov/pdf/321587.pdf

Abaqus References
For additional information on the Abaqus capabilities referred to in this brief, please see the following Abaqus 6.11 references:

 ‘Eulerian analysis,’ Section 14.1.1 of the Abaqus Analysis User’s Manual


About SIMULIA
SIMULIA is the Dassault Systèmes brand that delivers a scalable portfolio of Realistic Simulation solutions including the Abaqus prod-
uct suite for Unified Finite Element Analysis, multiphysics solutions for insight into challenging engineering problems, and lifecycle
management solutions for managing simulation data, processes, and intellectual property. By building on established technology, re-
spected quality, and superior customer service, SIMULIA makes realistic simulation an integral business practice that improves prod-
uct performance, reduces physical prototypes, and drives innovation. Headquartered in Providence, RI, USA, with R&D centers in
Providence and in Suresnes, France, SIMULIA provides sales, services, and support through a global network of over 30 regional
offices and distributors. For more information, visit www.simulia.com

The 3DS logo, SIMULIA, Abaqus and the Abaqus logo are trademarks or registered trademarks of Dassault Systèmes or its subsidiaries, which include Abaqus, Inc. Other company, product and service
names may be trademarks or service marks of others.
Copyright Dassault Systèmes, 2009

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Earth Penetration Simulation using Coupled Eulerian-Lagrangian Analysis

  • 1. Abaqus Technology Brief TB-09-PEN-1 Revised: July 2009 Earth Penetration Simulation using Coupled Eulerian-Lagrangian Analysis Summary In earth penetration events the projectile generally strikes the target at an oblique angle. As a result, the projectile is subjected to a multi-axial force and acceleration history through impact. The effectiveness of an earth penetration system is enhanced by the ability to withstand severe lateral loading. Consequently, it is important to under- stand how such loads develop during an impact event. In this Technology Brief, Abaqus/Explicit is used to simu- late the impact of a high-strength steel penetrator into a concrete target. The penetrator/target interaction is ana- lyzed using the coupled Eulerian-Lagrangian methodol- ogy. Specifically, the penetrator is modeled in a tradi- tional Lagrangian framework while the concrete target is modeled in an Eulerian framework. It will be shown that Abaqus/Explicit results are in good agreement with pub- lished experimental data. Click to animate Background Key Abaqus Features and Benefits The in-service accelerations that an earth-penetrating projectile experience can depend on the obliqueness of  Coupled Eulerian-Lagrangian capability allows the impact. As the impact condition deviates from the limiting general contact interaction of Eulerian and La- case of being perfectly normal to a flat surface, the accel- grangian regions of a model, simplifying the simu- erations lateral to the projectile’s body axis increase. lation of the extreme deformation associated with impact events It is well known that such ‘non-normal’ impact conditions produce large lateral forces and accelerations that can  Concrete damaged plasticity model simulates threaten the survivability of the penetrator case and inter- damage due to complex stress states nal components [1]. Clearly, a predictive capability that allows for simulation of an oblique impact penetration  Accelerometer connector elements measure ac- event provides the means to better design earth penetrat- celerations in a body-fixed coordinate system ing systems.  Anti-aliasing run-time filters simplify the removal A high-speed impact event very often involves extreme of noise from results states of deformation and/or material failure. A traditional Lagrangian finite element approach, in which elements tor impacting concrete. As outlined in [1], a series of ex- deform as the associated material deforms, is limited in periments was undertaken in which concrete test targets the extent of deformation an element can sustain. An Eul- were subjected to penetrator impacts at different angles erian formulation differs however, in that material flows of obliquity. The recorded acceleration results will be through a mesh of nodes that remain fixed in space; the compared to those of an Abaqus/Explicit analysis, in Eulerian framework is thus ideally suited for analyses that which the penetrator is modeled with Lagrangian ele- involve extreme levels of deformation, up to and including ments and the concrete is modeled as an Eulerian mate- material failure and rupture. Abaqus/Explicit allows full rial. coupling of Lagrangian elements and Eulerian material domains in an analysis through simple general contact Analysis Approach definitions. The penetration test under consideration is illustrated in This Technology Brief considers the coupled Eulerian- Figure 1. The concrete target is of a cylindrical shape Lagrangian (CEL) analysis of high-strength steel penetra- and is cast in a thin-walled steel pipe. It is cut to an angle
  • 2. 2 The objective is to create a mesh that is adequately re- fined near the contact zone while keeping the total num- ber of elements to a minimum. To achieve this goal, the mesh resolution is biased in such a way that the mesh becomes coarser away from the contact zone. A mesh refinement study was conducted, and a uniform grid spac- ing of 5 mm in the immediate area of impact was found satisfactory. This 5 mm grid extends out uniformly in both in-plane directions for about 5 projectile diameters, be- yond which the grid is graded out to the boundaries. In the direction of penetration, a uniform mesh with a 5 mm resolution is used. The final Eulerian mesh consists of approximately 1 million elements. The duration of the dy- namic analysis is 7 milliseconds. Figure 1: Cross-sectional schematic view of test configu- To measure acceleration, an accelerometer-type connec- ration tor element is placed at the center of the acceleration re- cording device (shown in Figure 2). This type of connector of 30 degrees with the cylinder axis. provides a convenient way to measure acceleration in a coordinate system fixed to a moving body. Figure 2 shows the cross section of the projectile used in the test. Its case is made of 4130 steel.  During the test, a Material Models smooth-bore powder gun launched the projectile with a striking velocity of 334 m/s.   The direction of the impact The concrete damaged plasticity model is used to capture velocity was aligned with the axis of the cylinder such that the constitutive behavior of the concrete. With the inclu- the angles of pitch and yaw (i.e. the amount of misalign- sion of multi-hardening plasticity and isotropic damaged ment between the velocity and projectile axes) were both elasticity, the model is ideal for applications where con- less than one degree and could be safely neglected. crete is subject to monotonic, cyclic or dynamic loading. The projectile’s acceleration was measured with a forward It assumes that the two main failure mechanisms are ten- mounted accelerometer that collected data at sile cracking and compressive crushing. For this analysis, 10μs intervals. The data was filtered with a two-pass, four- the associated data were derived from hydrostatic and pole Butterworth filter with a cutoff frequency of 2 kHz. shear failure envelopes given in [1]. While not included in this analysis, the effect of strain-rate dependence can be Finite Element Model added for an even higher level of fidelity. The full three-dimensional projectile is modeled with ap- The penetrator case, steel pipe, and penetrator internal proximately 13,000 Lagrangian hexahedral reduced- components are modeled with linear elastic materials. integration elements. The target is modeled with an Eule- This is based on the assumption that the amount of abra- rian mesh, including both the concrete and the thin-walled sion and erosion of the penetrator nose is small and the steel pipe. The Eulerian mesh is extended beyond the initial volume of concrete so that fragments created during impact are accounted for. A cross section of the assem- bled model is shown in Figure 3. Figure 3: Cross section of assembled coupled Eulerian- Figure 2: Cross-sectional view of projectile Lagrangian model
  • 3. 3 penetrator wall does not yield. The material properties for the internal components were chosen such that the cor- rect penetrator weight and moments of inertia were achieved. Contact Interactions and Loadings The interaction between the Eulerian target and Lagran- gian penetrator is handled through the general contact capability in Abaqus/Explicit, which automatically detects and resolves contact interactions. Results The primary quantities of interest from the test are the axial and lateral projectile accelerations, the depth of penetration, and the rest (turning) angle.   Figure 5: Depth of penetration and rest (turning) angle Acceleration histories direction (Figure 2). This makes the axial deceleration of The time history plot of both the axial (blue) and lateral the projectile positive. The lateral acceleration direction is (green) accelerations is shown in Figure 4. Both the test aligned with the negative global Y direction. (dashed) and the simulation (solid) results are shown. Good correlation is observed between the test and simu- The axial acceleration profile in Figure 4 shows that from lation results, with peak acceleration difference less than initial impact until the penetrator nose is buried, the decel- 5%. eration  increases. After that, the deceleration decreases in the general trend of the experimental data. Simulation of high-speed impact events with explicit finite element schemes is known to produce noisy results. Anti- Initiated by asymmetric loads (due to the oblique impact) aliasing filters are provided in Abaqus (during run time in during nose burial, the penetrator pitches upward and the solver phase or in the post-processing phase) to con- eventually the tail impacts the side of the hole created by veniently filter the noise. The acceleration data shown in the burrowing penetrator. The bending of the beam-like Figures 4 and 6 have been filtered using a sine- penetrator body due to the large inertial loading immedi- Butterworth filter with a cutoff frequency of 2 kHz. ately after the initial impact exacerbates this “slap-down” process. The effect from this significant short-duration To be consistent with the experimental setup, the axial lateral loading is evident in the lateral acceleration profile acceleration direction is aligned with the negative global X in Figure 4. As the event progresses, secondary lateral loads continue to produce peaks in the profile as the penetrator body contacts the sides of the hole. Depth of Penetration Results for the final depth of penetration and the rest (turning) angle are shown in Figure 5 and Table 1. As with the acceleration results, there is good correlation between the test and the simulation. Figure 6 contains an animation that provides a synchronized view of the penetration defor- mation and the acceleration time history. Note that the peak von Mises stress shown is well below the yield strength of 1345 MPa for the 4130 steel penetrator case, except in the region near the nose where localized erosion is ex- pected and was actually observed during the test. Nose Tip Nose Tip Path X'‐Y' X' Y' Length Rest Angle (m) (m) (m) (degrees) Test 0.62 0.69 0.93 43.0 FEA 0.60 0.80 1.00 36.9 Figure 4: Comparison of Abaqus/Explicit and measured Table 1: Path length and rest angle results and measure- acceleration histories. Note that deceleration is positive. ments
  • 4. 4 Figure 6: Synchronized animation of deformation, acceleration time histories, and von Mises stress in penetrator case. Click to animate Summary approach correlate very well with the chosen experimen- A coupled Eulerian-Lagrangian finite element based ap- tal data and demonstrate the utility of the coupled ap- proach to the simulation of earth penetration events is proach to modeling high-speed impact events that involve demonstrated using Abaqus/Explicit. The results from this material damage and extreme levels of deformation. References 1. Stokes, E., Yarrington, P. and Glenn, L., “An Earth Penetration Modeling Assessment: Prediction of Lateral Loading for Oblique Impact Conditions”, UCRL-TR-213206, Lawrence Livermore National Laboratory, Livermore, California, 2005. https://e-reports-ext.llnl.gov/pdf/321587.pdf Abaqus References For additional information on the Abaqus capabilities referred to in this brief, please see the following Abaqus 6.11 references:  ‘Eulerian analysis,’ Section 14.1.1 of the Abaqus Analysis User’s Manual About SIMULIA SIMULIA is the Dassault Systèmes brand that delivers a scalable portfolio of Realistic Simulation solutions including the Abaqus prod- uct suite for Unified Finite Element Analysis, multiphysics solutions for insight into challenging engineering problems, and lifecycle management solutions for managing simulation data, processes, and intellectual property. By building on established technology, re- spected quality, and superior customer service, SIMULIA makes realistic simulation an integral business practice that improves prod- uct performance, reduces physical prototypes, and drives innovation. Headquartered in Providence, RI, USA, with R&D centers in Providence and in Suresnes, France, SIMULIA provides sales, services, and support through a global network of over 30 regional offices and distributors. For more information, visit www.simulia.com The 3DS logo, SIMULIA, Abaqus and the Abaqus logo are trademarks or registered trademarks of Dassault Systèmes or its subsidiaries, which include Abaqus, Inc. Other company, product and service names may be trademarks or service marks of others. Copyright Dassault Systèmes, 2009