Research Article Impact Factor: 4.226 Yashasvi Giridhar, IJPRET, 2015; Volume 3 (9): 104-111 ISSN: 2319-507X IJPRET INTERNATIONAL JOURNAL OF PURE AND APPLIED RESEARCH IN ENGINEERING AND TECHNOLOGY A PATH FOR HORIZING YOUR INNOVATIVE WORK A QUALITATIVE ANALYSIS OF DYNAMIC AXIAL CRUSHING OF THIN WALLED SQUARE COLUMNS YASHASVI GIRIDHAR, MOHD. ZAHID ANSARI PDPM-Indian Institute of Information Technology, Design and Manufacturing Jabalpur, Khamaria, Jabalpur, MP, India 482005 Accepted Date: 05/03/2015; Published Date: 01/05/2015 Abstract: The axial crushing phenomenon of dynamically loaded thin walled columns provides an efficient means to improve the impact energy absorption and crashworthiness of automotives. This work uses a finite element analysis to study the crushing of square aluminium alloy tubular columns under dynamic load conditions. A mass of 400 kg moving at two different velocities was used to apply the dynamic loads. The side length and wall thickness of columns were changed to study their effect of crushed length and plastic strain energy stored during the crushing. Finally, a qualitative analysis was performed over the obtained results in comparison with super folding element theory. Keywords: Column; nonlinear dynamics; crash worthiness; super folding element theory; progressive dynamic collapse. \ Corresponding Author: MR. YASHASVI GIRIDHAR Access Online On: www.ijpret.com How to Cite This Article: PAPER-QR CODE Yashasvi Giridhar, IJPRET, 2015; Volume 3 (9): 104-111 Available Online at www.ijpret.com 104 Research Article Impact Factor: 4.226 Yashasvi Giridhar, IJPRET, 2015; Volume 3 (9): 104-111 ISSN: 2319-507X IJPRET INTRODUCTION Thin walled metal columns have been a source of interest for a long time owing to their high impact energy absorbing characteristics as well as their well defined collapse patterns. Due to their high energy absorption capacity coupled with lighter weight they have been widely used in automotive industry such as in cars and trains to not only provide high structural integrity but also high crash worthiness. To improve their energy absorption ability, grooves [1], dents [2] and pre-folds [3, 4] can be introduced to reduce the initial buckling load. The columns normally have tubular profile with square, rectangular or circular section. Square and rectangular forms are normally used in trains whereas the circular ones are more commonly used in landing gears in airplanes and helicopters where the telescopic tubular arrangement can also impart good vibration absorption feature to it. The buckling and collapse of a circular tube column under axial compressive load shows various collapse modes depending on tube width-to-thickness ratio. Short and thin square tubes are commonly used in energy absorption mechanisms for their easy collapsing features, usually collapse in the symmetric mode [4]. Many efforts have been made in understanding the collapse pattern of thin walled tubes with different cross sections with emphasis on higher energy absorption capacity. Wierzbicki and Abramowicz [5] presented a simple theoretical model called basic or super folding element (SFE) to predict the collapse behaviour of tubular structures loaded axially. This element consisted of four folding surfaces, i.e. conical, cylindrical, trapezoidal and toroidal surfaces, and the element is circumferentially in-extensional. The energy dissipation in SFE in affected by the stationary plastic hinge lines, the travelling plastic hinge line and the associated localized in-plane stretching of the toroidal surface. It was found that travelling plastic hinge lines were most effective in energy dissipation [5]. The material properties are considered here to be rigid-perfectly plastic with a constant value of the flow stress. This paper aims to investigate the crushing behaviour of thin walled tubular square aluminium alloy columns under axial compressive load. The height of the columns was fixed and its side length and wall thickness were varied. The columns were subjected to a dynamic load of 400 kg mass moving at velocities 7.5 m/s and 15 m/s, respectively. A commercial finite element analysis software LS-DYNA Explicit was used to simulate the collapse deformation behaviour of the columns. The collapse mechanism and the energy absorption characteristics of the columns are studied. Available Online at www.ijpret.com 105 Research Article Impact Factor: 4.226 Yashasvi Giridhar, IJPRET, 2015; Volume 3 (9): 104-111 ISSN: 2319-507X IJPRET 2. Theory and Modelling The buckling and collapse behaviour of tubular columns can be into classified into three types, i.e. static plastic buckling, dynamic plastic buckling and dynamic progressive buckling. In crash scenarios of automotive chassis, generally this behaviour lies in the region of dynamic plastic buckling and dynamic progressive buckling. In addition, it also depends on factors such as initial impact velocity, mass ratio between the impact mass and the tube. The deformation mechanics involved in all these is similar. The large plastic deformations are accommodated by the formation of complicated pattern of folds and wrinkles in the thin wall of the columns. During this collapse process, fold lines are formed continuously and bending occurs, leading to formation of double curvature surfaces. The basic plastic folding mechanism consists of five different deformation steps: (1) deformation of a floating toroidal surface (2) bending along stationary hinge lines (3) rolling deformations (4) opening of a conical surface and (5) bending of deformations along inclined stationary hinge lines which follow the locking of travelling hinge line as mentioned in step 3. SFE was proposed taking into consideration the material continuity and kinematic admissibility criteria. The deformation mode consisting of four trapezoidal elements, a section of two horizontal cylindrical surfaces, two inclined conical surfaces and a section of a toroidal surface is called the basic folding mechanism. The mean crushing force (Pm) for a thin walled square column can be given as [6,7]: Pm 13.06 0 b 1/3 t 5/3 (1) where, σ0 is flow stress of the column material and b and t are the side length and the wall thickness of the square column. For elastic-strain hardening materials with power law hardening behaviour, flow stress can be given as [8]: 0 y u 1 n Where, σy is yield stress and σu is tensile strength, and n is power law exponent. 3. Finite Element Analysis Figure 1 shows the schematic design of the thin square columns used in this study. The height of the column was fixed at 300 mm but its side length was changed as 30 mm and 60 mm and its wall thickness as 1.5 mm and 3 mm. The crash conditions were simulated as a mass of 400 kg Available Online at www.ijpret.com 106 Research Article Impact Factor: 4.226 Yashasvi Giridhar, IJPRET, 2015; Volume 3 (9): 104-111 ISSN: 2319-507X IJPRET striking the top, free-end of the square columns at two different velocities as 7.5 m/s and 15 m/s. Thus, in total 8 cases were studied. The bottom end of the columns was fixed to a rigid base. The columns were made of aluminium alloy and its material properties are listed in Table 1. Fig.1 Schematic of thin square column. Table 1 Mechanical properties of aluminium alloy Properties Young’s modulus (GPa) Density (kg/m3) Poisson’s ratio Yield stress (MPa) Tangent modulus (MPa) Al 71 2770 0.33 280 500 The crash simulations were conducted using a commercial finite element analysis software LSDYNA. The column material was considered as piecewise linear plasticity material with bilinear isotropic hardening. The mechanical properties of the column material are listed in Table 1. The finite element models were meshed using shell elements. This was done to reduce the computational time required as well as for better predictions as compared to usual solid elements in the case of thin walled structures. The shell elements chosen were the full integration 4-node Belytschko-Tsay elements. The boundary conditions were chosen to simulate the impact of a heavy mass over the top surface of the tubes that remained in contact throughout the transient phase of deformation. This was achieved using mass elements of 400 Available Online at www.ijpret.com 107 Research Article Impact Factor: 4.226 Yashasvi Giridhar, IJPRET, 2015; Volume 3 (9): 104-111 ISSN: 2319-507X IJPRET kg added to the topmost nodes of the columns and these nodes were initialised with the deforming loads in form of kinetic energy velocities. The complete impact time was set to be 10 ms over which the entire crash analysis was made. This short duration over which heavy loads were applied ensured that the dynamic effect of inertia was activated as opposed to the quasi static conditions of collapse. 4. RESULTS AND DISCUSSION Figure 2 shows the finite element results for a typical crushing sequence behaviour at different time steps in the aluminium alloy square columns under the impact load. The entire crash time was 10 ms. Both solid and wireframe results are shown to illustrate the buckling and collapse behaviour by observing the folding mechanism and its propagation. Fig.2 Solid (left) and wireframe (right) deformed shapes of the axially crushed square aluminium alloy tube column at different time steps. Figure 3 shows crushed length or the reduction in total height of the square columns under the dynamic impact load of 400 kg mass moving at 7.5 m/s and 15 m/s, respectively. The initial height of the columns was 300 mm. It can be seen in the figures that crushed length is decreased with increase in column wall thickness and side lengths, which indicates the Available Online at www.ijpret.com 108 Research Article Impact Factor: 4.226 Yashasvi Giridhar, IJPRET, 2015; Volume 3 (9): 104-111 ISSN: 2319-507X IJPRET increased resistance offered by the columns to buckling and crushing. This observation is consistent with the relation given by Eq. 1. It can also be observed in the figures that the crushed length is more than doubled when the impact velocity is doubled from 7.5 m/s to 15 m/s. It should be noted that the strain-hardening property of the aluminium alloy is already included and implemented by the finite element software used in this study [9]. Fig.3 Crushed length in different (b, t) square aluminium alloy columns for impact velocity 7.5 m/s (left) and 15 m/s (right) at 10 ms. Figure 4 shows the plastic energy stored in the square columns due to the plastic deformation under the dynamic impact load of 400 kg mass moving at 7.5 m/s and 15 m/s, respectively. The kinetic energy of the moving mass in converted into elastoplastic strain energy and the resulting deformation in the columns. The deformation occurs in form of localized buckling and fold formation which lead to collapse and crushing of the columns. Fig.4 Plastic strain energy stored in different (b, t) square aluminium alloy columns for impact velocity 7.5 m/s (left) and 15 m/s (right) at 10 ms. Figure 5 show the effective plastic strain contour plot in the deformed square aluminium alloy columns for different side lengths and wall thicknesses when crushed by a mass of 400 kg striking axially at, respectively, 7.5 m/s and 15 m/s. Red indicates maximum plastic deformation, whereas, blue represents the minimum or no plastic deformation. The plastic Available Online at www.ijpret.com 109 Research Article Impact Factor: 4.226 Yashasvi Giridhar, IJPRET, 2015; Volume 3 (9): 104-111 ISSN: 2319-507X IJPRET folding mechanism can easily be observed in the figures. The local buckling and first folds generally started at the bottom of the columns triggering further buckling and collapse of the column. Fig.5 Effective plastic strain in different (b, t) deformed square aluminium alloy columns at impact velocity 7.5 m/s (top row) and 15 m/s (bottom row) at 10 ms. 5. CONCLUSIONS In this paper we studied the crash behaviour of square thin walled tubes under dynamic load. The effect of different column designs and impact velocities were studied using finite element software. Results showed good conformity to the deformation mechanisms predicted by super folding element theory. The crushed length of the columns decreased with increase in wall thickness and side length. In addition, doubling the impact velocity more than doubled the crush length. Since the increase in column side length and wall thickness increased its resistance to buckle, the plastic energy stored due to the permanent deformation of the columns also increased. The real-time study of crushing sequence found that the crushing and the first folding generally started at the bottom of the columns and the consequent fold then propagated upwards and piled over it. ACKNOWLEDGEMENT This study was supported by PDPM-IIITDM-Jabalpur. Available Online at www.ijpret.com 110 Research Article Impact Factor: 4.226 Yashasvi Giridhar, IJPRET, 2015; Volume 3 (9): 104-111 ISSN: 2319-507X IJPRET REFERENCES 1. Mamalis, A. G., Manolakos, D. E., Viegelahn, G. L., Vaxevanidis, N. M., and Johnson, W., 1986, “The Inextensional Collapse of Grooved Thin-Walled Cylinders of PVC Under Axial Loading,” Int. J. Impact Eng., 4(1), pp. 41–56. 2. Lee, S., Hahn, C., Rhee, M., and Oh, J. E., 1999, “Effect of Triggering on the Energy Absorption Capacity of Axially Compressed Aluminium alloy Tubes,” Mater. Des., 20(1), pp. 31–40. 3. Langseth, M., Berstad, T., Hopperstad, O. S., and Clausen, A. H., 1994, “Energy Absorption in Axially Loaded Square Thin-Walled Aluminium alloy Extrusions,” Structures Under Shock Impact III(SUSI III), CMP, Southampton, pp. 401–410. 4. Jiayao Ma and Zhong You, Energy Absorption of Thin-Walled Square Tubes With a Prefolded Origami Pattern—Part I: Geometry and Numerical Simulation, Journal of Applied Mechanics, 2014, Vol. 81 / 011003-1 5. Wierzbicki, T., and Abramowicz, W., 1983, “On the Crushing Mechanics of Thin-Walled Structures,” ASME J. Appl. Mech., 50(4), pp. 727–734. 6. Abramowicz, W., and Jones, N., 1984, “Dynamic Axial Crushing of Square Tubes,” Int. J. Impact Eng., 2(2), pp. 179–208. 7. Abramowicz, W., and Jones, N., 1986, “Dynamic Progressive Buckling of Circular and Square Tubes,” Int. J. Impact Eng., 4(4), pp. 243–270. 8. Santosa, S., and Wierzbicki, T., 1998, “Crash Behavior of Box Columns Filled With Aluminum Honeycomb or Foam,” Comput. Struct., 68(4), pp. 343–367. Available Online at www.ijpret.com 111
© Copyright 2024