In an optimal design, more often than not, an initial configuration of a structure must be modified several times to provide the optimal arrangement. The objective of the project is to develop and use...

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In an optimal design, more often than not, an initial configuration of a structure must be modified several times to provide the optimal arrangement. The objective of the project is to develop and use a genetic algorithm to find such as arrangement for multi-layered shields.


When the nature of loading is known, systematic optimisation methods such as genetic algorithm could help find the best solution through an iterative process. It is therefore essential to use a robust optimisation scheme along with prior knowledge of the nature of loading on the structure to provide a heuristic algorithm to solve for best response. A plate of a given thickness (t) subjected to a particular ballistic threat has a certain ballistic limit (V50) and offers certain level of energy absorption. If the same plate is replaced by a set of plates of thicknesses t1 to tN , where N denotes the number of layers, in such a way that t=t1+t2+…tN, one can increase ballistic limit and energy absorption through correct selection of N-1 independent thickness variables for the same weight of the system.




DEPARTMENT OF MECHANICAL & AEROSPACE ENGINEERING Module Code: ME3309-ME3399 Module Title: Major Individual Project Module Leader: Mrs Petra Gratton Assessment Title: Project Proposal and Methodology Report Module Weighting: 15% Ballistic impact response of multi-layered shields Sanjeet Shokeen Student ID: 1733044 Project supervisor: Dr Arash Soleiman Fallah Table of Contents Abstract3 1.0Aim of the project4 2.0Objectives of the project4 3.0Context of the project4 4.0Background to the project5 5.0Methods to be adopted in carrying out the project7 6.0Risk assessment10 7.0Project management10 8.0Ethical approval11 9.0Resource requirements11 10.0References12 Abstract Nomenclature: NIJ = National Institute of Justice NABIS = National Ballistics Intelligence Service VG = Vest Guard BLV = Ballistic Limit Value is the ballistic limit is the projectile constant determined experimentally is the density of the laminate is the static linear compression elastic limit is the diameter of the projectile is the thickness of the laminate is the mass of the projectile is the wave velocity is the young’s modulus is the bulk density C is the speed of light is the poisson’s ratio Aim of the project To create and train a heuristic algorithm to improve the ballistic limit of a multi-layered shield using Matlab and Ansys to obtain the best arrangement for ‘n’ no. of plates. This study aims to determine the energy absorption properties and Backface signature of a material. Objectives of the project The objectives to be met in order to reach the aim of this project are: · Obtain the best arrangement to increase the ballistic limit of ‘6’ multi-layered aluminium (Al6061) shields. · Obtain the best arrangement to increase the energy absorption capacity of ‘6’ multi-layered aluminium (Al6061) shields. · Obtain the best arrangement to minimise the Backface signature of ‘6’ multi-layered aluminium (Al6061) shields. · Reduce the manufacturing costs of aluminium (Al6061) multi-layered shields Context of the project In recent years, the ongoing threat of ammunition and explosively formed projectiles to civil and military structures has increased the need to optimise protective structures. (E.A. Flores-Johnson, 2011) There is an increased risk due to vast development in the manufacturing and technology of the projectiles which has raised concern to yield better armours and shields. Aluminium alloys have been the primary material of choice for the production of the fuselage, wing and other supporting structure for the commercial airliners and military cargo and transport since about 1930. (E.A.StarkeJr., 1996) Although, polymer matrix composites are used in the high-performance military aircraft Aluminium alloy is still the best choice for commercial and cargo transportation which makes this topic a subject of intensive research due to increased crime and violence in the world. Multi-layered shields are used in different places like School windows and doors, High Commissions and Embassies and other organisations where security and confidentiality are top priorities. These shields are also used to manufacture storage safes and a lot of other safety tools which makes it critical to further research and develop the technology. Although there are a lot of studies dealing with Ballistic response of multi-layered shields, their scope is limited when it comes to Aluminium Al6061 alloy with a spherical projectile. Hence it remains an open research topic since conclusive results of its effectiveness have not been obtained to date. This project makes a key contribution to the multi-layered shields technology. It helps to improve the technology by explaining the energy absorption effects of Aluminium Al6061 alloy and also creates the best arrangement for the plates to improve the ballistic limit whilst minimising the backface signature effects. Assumptions: In this project, 1. The material used is Aluminium alloy Al6061. 2. The shape of the projectile is spherical. 3. maximum of 6 plates will be used to match the total thickness. Limitations: 1) This project does not include the practical testing of the configuration obtained for Aluminium Al6061 multi-layered shield. Results and conclusion solemnly rely on the 3-D Numerical simulations performed using Ansys. 2) A particular ballistic threat with a spherical velocity and response of a multi-layered Aluminium Al6061 shield with a maximum of 6 plates to match the total thickness have been studied. Background to the project Introduction This project includes detailed analytical, numerical and simulated investigation to illuminate changes of the order of the plates of different thickness on the ballistic performance of aluminium shields at high-speed impact and studies dealing with analytical methods for the optimization of multi-layered aluminium shields. Important features of this project are that · It gives a detailed explanation and simulation results of a high-speed spherical projectile impact response on a multi-layered aluminium shield with changing the order of the plates. Although, there are many studies available on Ballistic impact response none of them covers the response of aluminium with a spherical projectile which makes this topic open for further research. · This study will help reduce the manufacturing cost of multi-layered shields by educating manufacturers on the best arrangement for the shield and also reducing the material used. The project also focuses on keeping the cost minimum during the testing phase of multi-layered shields as it helps a lot to reduce overall the cost of the product. It focuses on delivering the testing results as quick as possible to minimise the time consumption. · Results from the analysis carried out will be helpful to understand the behaviour of aluminium multi-layered shields when stroked against spherical projectiles as it provides a detailed explanation and 3-D figures and numerical simulations. · It helps to increase the strength of the components made out of aluminium alloys like an aircraft fuselage, wings and many other parts by providing a better arrangement of multi-layered shields which can be used by manufacturers to produce better designs and structures. 4.2 NIJ Testing: (E.Frank, 1986) · Two different types of Ballistic tests are utilised to test the armour’s performance. The first test is the backfire signature test which calculates the performance of the armour against blunt force trauma and perforation. During the test, if single round penetrates the panel the structure is deemed to fail. It is carried out using clay where clay backing material must be less than 44mm. · The second type of testing conducted is ballistic limits deformation tests which measure its ballistic performance. Here multiple panels can be used to complete the tests. The testing velocity for subsequent projectiles varies depending upon the previous impact. Armours are tested for thermal conditions and also in submerged conditions to test the durability and capacity. · To keep improving the technology of multi-layered shields and armours it is important to research more and carry out experiments for a strong understanding of ballistic limit dynamics and energy absorption. 4.3 Existing Literature: Previous studies show that For the shields consisting of several plates with the same density but having different values of distortion pressure perforated, Ballistic limit value (BLV) of the armour can be increased if two adjacent plates are placed in a way such that value of the distortion pressure for the first plate is smaller than that of the second plate. The maximum ballistic limit value of armour is achieved when plates are arranged in increasing order of their distortion pressure values and minimum ballistic limit value is achieved when plates are arranged in their decreasing order of distortion pressure values. (G.Ben-Dor, 2014) Following case studies provide the results and conclusion for experiments carried out in past. 1) Penetration resistance of double-layered sheet structures: (Nysmith, 1968) · Small Pyrex glass spherical projectiles were made to strike into aluminium double-layered sheet at velocity 8.8Km/s to determine the effects of total sheet thickness and sheet spacing upon penetration resistance. · The Ballistic limit for two equally thick Al sheets was found to increase with an increase in total sheet thickness and sheet spacing. · In addition, the effectiveness of sheet spacing increase with the increase in projectile velocity whilst keeping the ratio of total sheet thickness to projectile diameter fixed. · It was determined that front-sheet hole diameter varies with the square root of the impact velocity. · It was concluded that at a given velocity the ratio of front sheet thickness to projectile causing maximum vaporization will be used as thickness for front sheet and remaining mass in the rear sheet for most efficient double-layered structure. 2) Ballistic performance of multi-layered metallic plates impacts by a 7.62-mm APM2 projectile. (E.A. Flores-Johnson, 2011) · An investigation was conducted to the test the Ballistic performance of monolithic, double and triple-layered metallic plates made of aluminium or steel or a combination of both. · The test shows that monolithic plates have a better ballistic performance than that of multi-layered plates made out of the same material. · Double layered plates with a thin front plate of aluminium and thick back steel plate exhibit greater resistance than multi-layer steel plates with similar area density. · It was concluded that further research should be carried out on the multi-layered target using different metallic material for better ballistic performance and weight savings. · They also found that reduction of resistance in multi-layered targets become more apparent as the no of plates is increased keeping the total thickness of the plate constant. 3) New results on ballistic performance of multi-layered metallic shields: (G.Ben-Dor, 2017) · This survey includes the analytical, numerical and experimental studies in which the effect of layering, spacing and change of the order of the plates have been considered leading to the Ballistic limit of the metallic shields against high-speed projectiles. · It was concluded that there are number of parameters that affect the penetration like the shape of the projectile, velocity, material, impact position and many more. · Further investigation has to carried out to determine the penetration laws and prepare a pattern · For sharp projectiles, layering and spacing decrease the ballistic performance of the shields and order of plates made from different material in the multi-layer shield may have a significant effect on the shield ballistic properties. · For blunt projectiles, layering and spacing have a negative impact on ballistic resistance but a variation of the order of layers manufactured from the same material but having different thickness affects ballistic resistance of the shields. All these studies were tested in laboratory conditions with real projectiles and final manufactured shields. These studies provide the actual tested results and help in better understanding of the ballistic limits, resistance, projectile penetration and backfire signature. Methods to be adopted in carrying out the project 5.1Methodology · To begin with, the project data sets will be extracted from the known historic experimental records of ballistic impact responses for different projectiles. Using previous journals and papers to study the existing researches and collecting data for ballistic impact responses of aluminium alloy (Al6061) and spherical projectile. Energy absorption properties of aluminium are very important to understand as it helps to build structures and shields with the better ballistic limit. · ‘Matlab Genetic Algorithm’ will be used to analyse the data and create heuristic algorithms which
Answered Same DayApr 01, 2021

Answer To: In an optimal design, more often than not, an initial configuration of a structure must be modified...

Kshitij answered on Apr 06 2021
137 Votes
Methods
Various methods and approaches are being taken into account by the researchers to estimate and determine the best suitable method from the available alternatives, for the best suitable results and efficient outcomes. as in the past years, it has been noticed that the demand for accurate and reliable estimation and determination of the various low and high values of the performance of the various objects. The major objective of the same was to have a theoretical implication of the present practical methods. Here are the several methods undertaken to test the ballistic limitation of the machinery, they are as follows:
Lagrangian method
To understand the loss caused and the destruction occurred by the deformation of the aluminum sheets in the testing procedure is significant for ensuring the safety of the operations in the process of determination of the ballistic limit and checking the thickness and quality of the aluminum sheet against the factors creating pressure on the sheet
, threes separate methodologies were used for simulation purpose. In the various industries, it has been noticed that the practice of implementing the Johnson cook model is common and is incorporated into the most optimized fine material available with them. At the first and foremost stage of analysis, a 3D model was created in the system to check the ballistic limit of the sheet while applying the same level of pressure and force on the sheet as it will be facing practically. The presented model based on geometry shows that there consist an aluminum sheet as a target and the force of stanag is applied on the same with 37.62 * 54R AP ammunition. Before the core, a cap made up of lead-antimony was placed in front of the same. The major objective behind placing the cap was to stabilize the projectile at the time of flight and the very initial and starting stage of the penetration procedure.
The total mass applied on the sheet is approximately 10.04g. The velocity of the ammunition was noticed to be 854 m/s as stated in the stanag 4569. The simulation will make the use of the Lagrange method for the purpose of ammunition and to target the shield. At the time of generating the solution, two different types of appropriations were applied. In the first approach though the force applied was comparatively more but a small radius was generated in the shield to soften the same and to improve the ability of the sheet to bear the attacks and text the ballistic ability of the same. In the second model approach, the model was prepared in such a manner using the geometric approach for its presentation and preparation. Although, the prepared model of sine mesh was not that successful as per the expectations of the researchers, in the type first the domain of solution has not attained good correlation when compared to the results of the test. In the second type, because of the tetragonal mesh, and termination in the error, all this resulted in the distortion of the element. In order to eliminate the problems, the model was dismantled and redesigned with new features. The already generated model was optimized and modified in such a manner to maintain the stability of the results and to get the accurate and appropriate results for better performance. As in the conventional models, the numerical factor in the simulation was ignored by the researchers and only the accuracy and reliability of the same was taken as the significant areas for the study. The aluminum shield was divided into three major areas i.e. inner area middle area and outer area. The area is coarsening starting from the inner to the outer region. The transition among the different regions are good prominent enough to prevent the level of stress and will waive the reflections at the boundary area. The shield has meshed with constant hexagonal stress with various solid elements of numerous sizes ranging from 0.2 mm and 1 mm under total observe elements is approximately 734 in number. The projectile also reflects a very fine mess. The aluminum sheet includes 947 elements and 207 elements for the force applied to the same. Apart from the front and rear antimony caps, the properties of the JC model were being assigned to all the material present in the model. The antimony caps included in the model of various materials like ISOTROPIC etc. The algorithms that were implemented to simulate the connection among the surface at the time penetration. The option of erosion, static friction and dynamic and bucket frequency are investigated for an appropriate and accurate result. The parameters for control were also put to use to control hourglass, and for the purpose of terminating the solution. One of the most prominent and important tools for controlling the impact of the problem is the time step scale factor (TSSF). TSSF is the best available tool used for the purpose of providing optimum steps in time for the accuracy and confirmation of the numerical and geometrical stability (Fabre, Bonnet, et.al.,2017).
SPH method
In the year of 1983, Johnson and cook the most famous personalities of that period invented a model commonly known as Johnson cook model which created a mathematical equation which includes numerous phenomena like hardening the material, rate of hardening the same, and the process of thermal softening. However the same has t be clarified that their integrated effect is not taken into consideration. With the recent and constant level of developments, the SPH method has proved to be a reliable and efficient tool for the reason of providing accuracy and stability in the outcomes for the great problems like deformation and will result in successful implementation in the various hydro codes. One of the most common FE code which involves SPH is Ls-Dyna. In the recent studies because of the high cost in computation in SPH an alternative substitute for the numerical solutions the technique of combining FEM/SPH is being put to use. Since in the SPH method the use of the lagrangian formula is being implemented, integration of the SPH and lagrangian is possible with the help of defined interfaces in connecting the same. A similar kind of approach has been followed by various researchers in their study. The study of compatibility among the two different approaches i.e. SPF and Lagrangian solver in the process of Ls-Dyna is to ensure by permitting the use of the classical keywords and making the use of fixed approach comparatively convenient and easy. For resolving the issue, the section of large deformation of the objective id modeled along the SPH and where the deformation takes place in small sections of the society with the hexagonal lagrangian in the solid elements. Such combining and coupling should be optimistically arranged for the purpose of the simulate transition of the various propagation of the wave at the interface of SPH –Lagrange. It has been observed that the stress of wave propagation after the impact of force and pressure applied on the sheet it was plotted at different time steps. As shown there was no reflection of the transition at the mesh boundaries. For the purpose of the simulation, the Lagrange method was used for the hardened aluminum projectile, SPH, and discretization of an aluminum target.
The various layers of the aluminum sheet were divided into numerous regions. In the SPH section, an equispaced discretization was put to use. After the application of various substances and material also the result was not being able to improve the accuracy and effectiveness of the system and hence were removed and omitted. The geometrical details of the model as generated from the above sources were used for detailed analyses of the system. The core target of the model was SPH having the size of the particle as 0.2 mm and are surrounded by a Lagrange region with an element size of 0.5 mm and 1 mm. the connection between SPH and the Lagrange element was developed with the help of tide notes to surface the connection was being able to build even at the time of penetration through the applied force. In SPH simulation the bulk of viscosity was ignored. In the model FE, the state rule required at least four notes of SPH. Reduction in the number of SPH notes or particles will result in earlier or premature penetration of the particles of the sheet into FE mesh without having any properties of the material. Even in the integrated approach, the cost of computation of the SPH is superior as comparative lagrangian analysis (Liu, Zhang, et.al., 2017).

Kneubuehl method
The Johnson cook model is a pre model of empirical study and is the most common and widely used model among all. This deals with the theory of continuum mechanics that defines the dependent rates and inelastic and low flexible behavior of the solids especially the layers of aluminum sheets. This method works on the theory of probabilities and statistics. It has been considered from his point that the response of armor P (Vi) is the cumulative distribution function (CDF) of the impact of the pressure in the velocity which is just a random variable, which causes the perforation of the target. Though the general velocity Vi is just a continuous randomly opted variable. This particular method helps in the implementation of the previously discussed methods and strategies and with the help of such strategies and planning a successful experiment is being carried for testing the ballistic limit of the various layers of the aluminum shield used for making automobiles. The same level of pressure is applied on such shields to check the point at which the sheet will break down or get damaged so that the cures and solution for the same could be found and implemented. Therefore, for the purpose of estimation of the central tendency and perforation dispersion, methods opted to solve the issue were statistical mean (Vm) along with standard deviation (σ), the applicable formulae for the same are
Vm =
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