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International Journal of Latest Technology in Engineering, Management & Applied Science (IJLTEMAS)
Volume VI, Issue VIIIS, August 2017 | ISSN 2278-2540
www.ijltemas.in Page 42
Numerical Investigations on Blast Protection System
with Metallic Tube Core Sandwich Panels
K. Uma Maheswari
Assistant Professor, Prince Shri Venkateshwara Engineering College, Tamil Nadu, India
Abstract: - Effect of blast loads from explosion can be mitigated
by using thick armor systems that are often heavy and
significantly increase the self-weight of the structure. In the
design of structure for blast protection, sacrificial claddings
which consist of high energy absorbing elements are used. A
sandwich type protective structure consists of light weight core
which is often used for blast mitigation. The choice of core type
has an influence on the performance of sandwich panel. The
cores can be of wood, foam material and tubular elements. In
this study, behavior of sandwich panel with square tubular core
is investigatedthrough numerical studies. Panel is made of mild
steel having top plate dimension of 150 mm x 150 mm x 2.5 mm;
bottom plate of 150 mm x 150 mm x 5 mm and square tube core
of 12.5 mm x 12.5 mm with 0.6 mm thickness. A finite element
model is developed and validated using experimental results in
literature. Parametricstudies are carried out using the validated
finite element model. By varying the tube length of the core, the
responses of the panels in terms of energy absorption and
reaction forces are compared.
KEYWORDS: - Blast loading, Reaction forces, Tube core
sandwich panel, Energy absorption.
I. INTRODUCTION
he analysis and design of structures subjected to blast
loads require understanding of blast phenomena and
dynamic response of structural elements [1]. For blast
resistant structures efficient energy absorbing
material/structural configuration is preferred Sandwich panel
with honey comb, square, folded plate, pyramidal, corrugated
and diamond cores are commonly used as energy absorbers.
Sacrificial cladding layers are used for blast mitigation [2].
They have investigated both experimental and analytically the
sacrificial layered structure with mild steel web plates. The
cladding structures are mainly designed in such a way that the
forces transferred are controlled to an extent in the protective
structure. Core height and face plate thickness influences the
response of honeycomb sandwich panel [3]. Optimum mass
distributions for blast mitigation through sandwich plates are
investigated by maximizing the impulse capacity while
limiting the back face acceleration. Constraints in
development of protection system for existing structure
should not produce additional weight to the foundation [4]. By
varying the mass ratio between the face sheets and the core, it
influences the behavior of the sandwich panel [5].
Due to increase in absorption capacity of the protective layer,
the forces on the main structure may be reduced. Protective
layers with a large absorption capacity which transfer forces
less than the elastic limit of the primary structures are
preferred. In blast applications, buckling of a tube core will
limit the energy absorption capacity; the structural integrity of
primary structure may be compromised. Thus square tubes are
used as effective energy absorber. In this study, numerical
investigations are carried out by using the metallic tubular
elements in sandwich panel against blast loads. The main
objective of this investigation is to reduce the energy
transmission to the protected structure.
II. PROPERTIES
2.1 MATERIAL PROPERTIES
Mild steel is used for all the elements of the sandwich panel.
The stress strain data used in the simulation is obtained from
uni-axial tensile tests. The Young’s modulus is taken as 210
GPa and initial yield stress of the steel used in this study is
259 MPa. Mild steel exhibits linear elastic and strain
hardening behavior, subjected to plastic deformations.
According to Cowper-Symonds, the strain rate effect on mild
steel is obtained by Eqn (1).
[ ( )
⁄
] (1)
where σd – Dynamic yield stress
σo – Static yield stress
έ – Strain rate
D & q are material parameter where D = 844 s-1
and q = 2.207
which are found to be experimentally using locally available
steel [6].
Strain rates are taken based on the theoretical approximations
of the strain rate in the folding of square tubes. Density and
Poisson’s ratio of mild steel are taken as 7850 kg/m3
and 0.3
respectively. Specific heat of the panel is taken to be 452 J/kgº
C. Tangential friction is given as μk = 0.3[7].
2.2 GEOMETRICAL PROPERTIES
Panel geometry has a significant effect in energy absorbing
properties. The behavior of sandwich panel using square tubes
T
International Journal of Latest Technology in Engineering, Management & Applied Science (IJLTEMAS)
Volume VI, Issue VIIIS, August 2017 | ISSN 2278-2540
www.ijltemas.in Page 43
has been investigated in the presence of circular cutout in the
tube face. The cutout diameter is taken as the 1/4th
of the
mean width of the tube. These studies investigate the response
of panel structure by modifying the critical variables [8].
In this study, the top and bottom plate area is 150 mm x 150
mm. Tube size of 12.5 mm x 12.5 mm with thickness of 0.6
mm [9]. The variable λ = λ1 /λ2, where λ1 & λ2 are as shown in
Fig. 1, that defines position of the tube in the panel. Top plate
thickness of the panel is of 2.5 mmand bottomplate thickness
of panel is 5 mm. Fig. 1 shows the typical cross section of the
sandwich panel.
(a)
(b)
Fig. 1 Schematic diagram the sandwich panel (a) Elevation (b) Plan view
III. FINITE ELEMENT MODELLING
3.1 LOADING CONDITIONS
The modelling has been done in ABAQUS/CAE. The
characterization of blast load is defined using Eqn (2). The
equation represents the rectangular pressure pulse.
P(t) ={ (2)
where P0 is the peak pressure of the applied load and t0 is the
pulse duration.
Impulse is assumed to be I= 55Ns. The blast load applied is to
distribute uniformly in the form of pressure. The pulse
duration depends on the pressure exerted and the face plate
area and the corresponding setup is described in [8]. Pulse
duration t0 is calculated as 17.32μs [8]. The applied pressure is
calculated using the formulae P0 = I/At0. Fig. 2 shows the
loading pattern on the panel in the simulation.
3.2 BOUNDARY CONDITIONS
Boundary conditions of the panel have significant effect on
behavior of plates and tubes regarding buckling. Top plate is
free for all degrees of freedom and bottom plate is fixed in
space. The ends of the tube are clamped with both the plates
as in Fig. 2.
Fig. 2 Loading and Boundary conditions
3.3 MESHING
The panel is modeled using mesh elements in
ABAQUS/CAE. Bottom plate is fixed rigid. Top plate is
meshed using 8 noded brick element (C3D8R) and tube core
is meshed using 4 noded shell elements (S4R). Finite element
model of the panel is shown in Fig. 3.
Fig. 3 Finite element meshing of the sandwich panel
International Journal of Latest Technology in Engineering, Management & Applied Science (IJLTEMAS)
Volume VI, Issue VIIIS, August 2017 | ISSN 2278-2540
www.ijltemas.in Page 44
IV. VALIDATION OF RESULTS USING LITERATURE
Numerical model is validated with the response of the panel
available in literature [8] for blast load. The deformation
pattern of tube length of 50mm, 75mm, 100mm is shown in
Fig.4,5 & 6 respectively.
Deformation of the tube is 12% less when compared to that in
literature. By varying the tube length of the validated model it
is concluded that lesser the tube length more the deformation.
Energy absorption of the plate is predicted to be 10.58% more
when compared to that in literature and for tube it is predicted
that energy absorbed is approximately same.
Table 1 Results obtained from FEA
Description
Tube
deformation,
mm
Energy
Absorption, J
Plate Tube
Reference(Theobald et al.,
2007)
58.25 482 2700
Tube length of 75 mm 50.91 431.00 2722.26
(a)
(b)
Fig. 4 Deformationof 50mm tube length(a)Overall view(b) Closed view of
the tube
Fig. 5 Deformation of 75mm tube length
Fig. 6 Deformation of 100mm tube length
V. PARAMETRIC STUDIES
Parametric study is carried out varying the tube length to
50mm and 100mm. Variation of tube length is based on the
ratio of tube length to width ratio. This tube aspect ratio
ranges between 4 and 6. The geometric parameters used in the
study are chosen based on reasonable manufacturing and
experimental constraints.
Table 2 Variation in tube length
Parameter
Tube length /
Tube width
Value, mm
Tube length Tube width
Tube length
4
6
8
50
75
100
12.5
12.5
12.5
Table 3 Results from tube length variation
Tube length
(mm)
Tube
Deformation
(mm)
Energy
Absorption in
tube (J)
Mean
Reaction
Force (kN)
50 21.97 2650.12 16.44
75 50.91 2722.6 11.23
100 48.84 2878.4 13.80
International Journal of Latest Technology in Engineering, Management & Applied Science (IJLTEMAS)
Volume VI, Issue VIIIS, August 2017 | ISSN 2278-2540
www.ijltemas.in Page 45
Fig.7 Time variation of energy absorption
Fig.8 Time variation of reaction force at bottom plate
VI. CONCLUSION
Numerical investigations are carried out on sandwich panel
with tube cores. It is observed that the tube deformation,
energy absorption and reaction force at bottom plate varies
with change in tube length. The reaction force and tube
deformation are highly sensitive to the tube geometry. Energy
absorption is found to decrease with reduction of tube length.
Tube length of 100 mm shows lateral bucking instead of
crushing of tube core and also the reaction force is 18.64%
more when compared to 75 mm tube length. From the
numerical investigations, the panel having 75 mm tube length
is found to be more effective under an impulse of 55 Ns.
REFERENCES
[1]. T. Ngo, P. Mendis, A. Gupta & J.Ramsay.,2007, “Blast loading
andblast effects on structures”, EJSE special issue: Loading and
Structures
[2]. S. Guruprasad, A. Mukherjee.,2000, “Layeredsacrificial cladding
under blast loading”, International Journalof Impact Engineering.
Vol 24, pp. 957-973
[3]. Y. Chi, G. S. Langdon, G.N. Nurick.,2010, “The influence of Core
Height andFace Plate Thickness onthe Responseof Honeycomb
Sandwich Panels subjectedto blast loading”,Material and Design
Vol 31, pp. 1887-1899
[4]. Cho-Chung Liang, Ming-Fang Yang, Pin-Wen Wu., 2001,
“Optimum design of metallic corrugated core sandwich panel
subjected to blast loads”, International Journal of Impact
Engineering, Vol 28, pp. 825-861
[5]. Joseph A. Main, George A. Gaxonas., 2008, “Uniaxial Crushing
of sandwich plates under air blast: Influence of mass distribution”,
International journal of Solids and structures Vol 45, pp. 2297-
2321
[6]. Marias ST, Tait RB, CloeteTJ., 2004, “Material testing at high
strain usingthe split Hopkinson pressure bar. Latin Am J solids
Structure, pp. 319-39
[7]. Nannuci P. Marshall NS, Nurick GN., 1998 “A computational
investigation of the progressive buckling of square tubes with
geometric imperfections”,In: Lok TS., Editors.ThirdAsia-Pacific
conference onshock andimpact loads on structures under shock
and impact, pp. 155-168
[8]. M. D. Theobald, G. N. Nurick.,2010, “Experimental and
numerical analysis of tube core claddings under blast loads”,
International Journal ofImpact Engineering, Vol 37, pp. 333-348
[9]. N. Anandavalli, J. Rajasankar.,2014, “Effectiveness of tube core
sandwich panel in structural protection against blast loads”, 5th
International Congress on Computational Mechanics &
Simulation, pp.749-759
0
500
1000
1500
2000
2500
3000
3500
0.000 0.001 0.002
Energy(kJ)
Time(s)
Energy of tube
Tube length
of 50mm
Tube legth
of 75mm
Tube length
of 100mm
0
5
10
15
20
25
30
35
40
45
50
0 0.001 0.002 0.003
Tube length
of 50 mm
Tube length
of 75mm
Tube lenth
of 100 mm
Time (s)
Reactionforce(kN)
Reaction Force of tube

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Numerical Investigations on Blast Protection System with Metallic Tube Core Sandwich Panels

  • 1. International Journal of Latest Technology in Engineering, Management & Applied Science (IJLTEMAS) Volume VI, Issue VIIIS, August 2017 | ISSN 2278-2540 www.ijltemas.in Page 42 Numerical Investigations on Blast Protection System with Metallic Tube Core Sandwich Panels K. Uma Maheswari Assistant Professor, Prince Shri Venkateshwara Engineering College, Tamil Nadu, India Abstract: - Effect of blast loads from explosion can be mitigated by using thick armor systems that are often heavy and significantly increase the self-weight of the structure. In the design of structure for blast protection, sacrificial claddings which consist of high energy absorbing elements are used. A sandwich type protective structure consists of light weight core which is often used for blast mitigation. The choice of core type has an influence on the performance of sandwich panel. The cores can be of wood, foam material and tubular elements. In this study, behavior of sandwich panel with square tubular core is investigatedthrough numerical studies. Panel is made of mild steel having top plate dimension of 150 mm x 150 mm x 2.5 mm; bottom plate of 150 mm x 150 mm x 5 mm and square tube core of 12.5 mm x 12.5 mm with 0.6 mm thickness. A finite element model is developed and validated using experimental results in literature. Parametricstudies are carried out using the validated finite element model. By varying the tube length of the core, the responses of the panels in terms of energy absorption and reaction forces are compared. KEYWORDS: - Blast loading, Reaction forces, Tube core sandwich panel, Energy absorption. I. INTRODUCTION he analysis and design of structures subjected to blast loads require understanding of blast phenomena and dynamic response of structural elements [1]. For blast resistant structures efficient energy absorbing material/structural configuration is preferred Sandwich panel with honey comb, square, folded plate, pyramidal, corrugated and diamond cores are commonly used as energy absorbers. Sacrificial cladding layers are used for blast mitigation [2]. They have investigated both experimental and analytically the sacrificial layered structure with mild steel web plates. The cladding structures are mainly designed in such a way that the forces transferred are controlled to an extent in the protective structure. Core height and face plate thickness influences the response of honeycomb sandwich panel [3]. Optimum mass distributions for blast mitigation through sandwich plates are investigated by maximizing the impulse capacity while limiting the back face acceleration. Constraints in development of protection system for existing structure should not produce additional weight to the foundation [4]. By varying the mass ratio between the face sheets and the core, it influences the behavior of the sandwich panel [5]. Due to increase in absorption capacity of the protective layer, the forces on the main structure may be reduced. Protective layers with a large absorption capacity which transfer forces less than the elastic limit of the primary structures are preferred. In blast applications, buckling of a tube core will limit the energy absorption capacity; the structural integrity of primary structure may be compromised. Thus square tubes are used as effective energy absorber. In this study, numerical investigations are carried out by using the metallic tubular elements in sandwich panel against blast loads. The main objective of this investigation is to reduce the energy transmission to the protected structure. II. PROPERTIES 2.1 MATERIAL PROPERTIES Mild steel is used for all the elements of the sandwich panel. The stress strain data used in the simulation is obtained from uni-axial tensile tests. The Young’s modulus is taken as 210 GPa and initial yield stress of the steel used in this study is 259 MPa. Mild steel exhibits linear elastic and strain hardening behavior, subjected to plastic deformations. According to Cowper-Symonds, the strain rate effect on mild steel is obtained by Eqn (1). [ ( ) ⁄ ] (1) where σd – Dynamic yield stress σo – Static yield stress έ – Strain rate D & q are material parameter where D = 844 s-1 and q = 2.207 which are found to be experimentally using locally available steel [6]. Strain rates are taken based on the theoretical approximations of the strain rate in the folding of square tubes. Density and Poisson’s ratio of mild steel are taken as 7850 kg/m3 and 0.3 respectively. Specific heat of the panel is taken to be 452 J/kgº C. Tangential friction is given as μk = 0.3[7]. 2.2 GEOMETRICAL PROPERTIES Panel geometry has a significant effect in energy absorbing properties. The behavior of sandwich panel using square tubes T
  • 2. International Journal of Latest Technology in Engineering, Management & Applied Science (IJLTEMAS) Volume VI, Issue VIIIS, August 2017 | ISSN 2278-2540 www.ijltemas.in Page 43 has been investigated in the presence of circular cutout in the tube face. The cutout diameter is taken as the 1/4th of the mean width of the tube. These studies investigate the response of panel structure by modifying the critical variables [8]. In this study, the top and bottom plate area is 150 mm x 150 mm. Tube size of 12.5 mm x 12.5 mm with thickness of 0.6 mm [9]. The variable λ = λ1 /λ2, where λ1 & λ2 are as shown in Fig. 1, that defines position of the tube in the panel. Top plate thickness of the panel is of 2.5 mmand bottomplate thickness of panel is 5 mm. Fig. 1 shows the typical cross section of the sandwich panel. (a) (b) Fig. 1 Schematic diagram the sandwich panel (a) Elevation (b) Plan view III. FINITE ELEMENT MODELLING 3.1 LOADING CONDITIONS The modelling has been done in ABAQUS/CAE. The characterization of blast load is defined using Eqn (2). The equation represents the rectangular pressure pulse. P(t) ={ (2) where P0 is the peak pressure of the applied load and t0 is the pulse duration. Impulse is assumed to be I= 55Ns. The blast load applied is to distribute uniformly in the form of pressure. The pulse duration depends on the pressure exerted and the face plate area and the corresponding setup is described in [8]. Pulse duration t0 is calculated as 17.32μs [8]. The applied pressure is calculated using the formulae P0 = I/At0. Fig. 2 shows the loading pattern on the panel in the simulation. 3.2 BOUNDARY CONDITIONS Boundary conditions of the panel have significant effect on behavior of plates and tubes regarding buckling. Top plate is free for all degrees of freedom and bottom plate is fixed in space. The ends of the tube are clamped with both the plates as in Fig. 2. Fig. 2 Loading and Boundary conditions 3.3 MESHING The panel is modeled using mesh elements in ABAQUS/CAE. Bottom plate is fixed rigid. Top plate is meshed using 8 noded brick element (C3D8R) and tube core is meshed using 4 noded shell elements (S4R). Finite element model of the panel is shown in Fig. 3. Fig. 3 Finite element meshing of the sandwich panel
  • 3. International Journal of Latest Technology in Engineering, Management & Applied Science (IJLTEMAS) Volume VI, Issue VIIIS, August 2017 | ISSN 2278-2540 www.ijltemas.in Page 44 IV. VALIDATION OF RESULTS USING LITERATURE Numerical model is validated with the response of the panel available in literature [8] for blast load. The deformation pattern of tube length of 50mm, 75mm, 100mm is shown in Fig.4,5 & 6 respectively. Deformation of the tube is 12% less when compared to that in literature. By varying the tube length of the validated model it is concluded that lesser the tube length more the deformation. Energy absorption of the plate is predicted to be 10.58% more when compared to that in literature and for tube it is predicted that energy absorbed is approximately same. Table 1 Results obtained from FEA Description Tube deformation, mm Energy Absorption, J Plate Tube Reference(Theobald et al., 2007) 58.25 482 2700 Tube length of 75 mm 50.91 431.00 2722.26 (a) (b) Fig. 4 Deformationof 50mm tube length(a)Overall view(b) Closed view of the tube Fig. 5 Deformation of 75mm tube length Fig. 6 Deformation of 100mm tube length V. PARAMETRIC STUDIES Parametric study is carried out varying the tube length to 50mm and 100mm. Variation of tube length is based on the ratio of tube length to width ratio. This tube aspect ratio ranges between 4 and 6. The geometric parameters used in the study are chosen based on reasonable manufacturing and experimental constraints. Table 2 Variation in tube length Parameter Tube length / Tube width Value, mm Tube length Tube width Tube length 4 6 8 50 75 100 12.5 12.5 12.5 Table 3 Results from tube length variation Tube length (mm) Tube Deformation (mm) Energy Absorption in tube (J) Mean Reaction Force (kN) 50 21.97 2650.12 16.44 75 50.91 2722.6 11.23 100 48.84 2878.4 13.80
  • 4. International Journal of Latest Technology in Engineering, Management & Applied Science (IJLTEMAS) Volume VI, Issue VIIIS, August 2017 | ISSN 2278-2540 www.ijltemas.in Page 45 Fig.7 Time variation of energy absorption Fig.8 Time variation of reaction force at bottom plate VI. CONCLUSION Numerical investigations are carried out on sandwich panel with tube cores. It is observed that the tube deformation, energy absorption and reaction force at bottom plate varies with change in tube length. The reaction force and tube deformation are highly sensitive to the tube geometry. Energy absorption is found to decrease with reduction of tube length. Tube length of 100 mm shows lateral bucking instead of crushing of tube core and also the reaction force is 18.64% more when compared to 75 mm tube length. From the numerical investigations, the panel having 75 mm tube length is found to be more effective under an impulse of 55 Ns. REFERENCES [1]. T. Ngo, P. Mendis, A. Gupta & J.Ramsay.,2007, “Blast loading andblast effects on structures”, EJSE special issue: Loading and Structures [2]. S. Guruprasad, A. Mukherjee.,2000, “Layeredsacrificial cladding under blast loading”, International Journalof Impact Engineering. Vol 24, pp. 957-973 [3]. Y. Chi, G. S. Langdon, G.N. Nurick.,2010, “The influence of Core Height andFace Plate Thickness onthe Responseof Honeycomb Sandwich Panels subjectedto blast loading”,Material and Design Vol 31, pp. 1887-1899 [4]. Cho-Chung Liang, Ming-Fang Yang, Pin-Wen Wu., 2001, “Optimum design of metallic corrugated core sandwich panel subjected to blast loads”, International Journal of Impact Engineering, Vol 28, pp. 825-861 [5]. Joseph A. Main, George A. Gaxonas., 2008, “Uniaxial Crushing of sandwich plates under air blast: Influence of mass distribution”, International journal of Solids and structures Vol 45, pp. 2297- 2321 [6]. Marias ST, Tait RB, CloeteTJ., 2004, “Material testing at high strain usingthe split Hopkinson pressure bar. Latin Am J solids Structure, pp. 319-39 [7]. Nannuci P. Marshall NS, Nurick GN., 1998 “A computational investigation of the progressive buckling of square tubes with geometric imperfections”,In: Lok TS., Editors.ThirdAsia-Pacific conference onshock andimpact loads on structures under shock and impact, pp. 155-168 [8]. M. D. Theobald, G. N. Nurick.,2010, “Experimental and numerical analysis of tube core claddings under blast loads”, International Journal ofImpact Engineering, Vol 37, pp. 333-348 [9]. N. Anandavalli, J. Rajasankar.,2014, “Effectiveness of tube core sandwich panel in structural protection against blast loads”, 5th International Congress on Computational Mechanics & Simulation, pp.749-759 0 500 1000 1500 2000 2500 3000 3500 0.000 0.001 0.002 Energy(kJ) Time(s) Energy of tube Tube length of 50mm Tube legth of 75mm Tube length of 100mm 0 5 10 15 20 25 30 35 40 45 50 0 0.001 0.002 0.003 Tube length of 50 mm Tube length of 75mm Tube lenth of 100 mm Time (s) Reactionforce(kN) Reaction Force of tube