Autor: Niezgoda, T. - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Aluminium foam testing for impact energy absorption aims
Autorzy:: Niezgoda, T.
Miedzińska, D.
Powiązania:: https://bibliotekanauki.pl/articles/245628.pdf
Data publikacji:: 2009
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: aluminium foam
microstructure modelling
open cell foam
closed cell foam
Opis:: Aluminium foams are a new group of materials used for impact energy absorbing elements. They are light (typically 10-25% of the density of the metal they are made of) and stiff, and are frequently proposed as a light weight structural material. That is why they often are applied in automotive and transport industry solutions, for example as parts of bumpers. The methods of numerical modelling for open and closed cell aluminium foams are presented in the paper as well as closed and open cellfoam microstructure model. The numerical models of foam ideal microstructures created with shell finite elements are shown. The models were developed on the basis of Kefain tetrakaidecahedrons - structures consisting of six squares and eight hexagons. In the case of closed cell foams, the polyhedron with full walls was adopted. In the case of open cell foams the circle wholes were removed from polyhedron surfaces. Then the numerical analysis of a created models compressive test was carried out with the usage of LS Dyna computer code. The nonlinear procedures were applied. The results were analyzed in the scope of energy absorbing properties of aluminium foams.
Źródło:: Journal of KONES; 2009, 16, 3; 283-289
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 2.

Tytuł:: Investigation of energy-absorbing capabilities of flexible elements in the aspect of applied materials
Badania energochłonności elementów podatnych w aspekcie zastosowanych materiałów
Autorzy:: Barnat, W.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/241727.pdf
Data publikacji:: 2007
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: bezpieczeństwo transportu
elementy energochłonne
wpływ materiału na energochłonność
transport security
energy-absorbing element
influence of material on energy-absorbing capabilities
Opis:: The paper deals with the problem of improvement of transport security through application of additional elements absorbing the crash energy. Experimental tests and numerical simulations of basic energy-absorbing elements in a shape of a sleeve made of steel, duralumin, bronze and glass-epoxy composite were presented. The results of the investigation will be used to develop a reliable numerical model of a panel of protective elements. The numerical analysis was carried out by the Finite Element Method using the DYTRAN code. The calculations were verified experimentally on a universal testing machine INSTRON in the Department of General Mechanics of the Military University of Technology. On the basis of results of numerical and experimental investigations it was found that the composite sleeves have the specific absorbed energy twice higher than the steel ones. An interesting supplement of the energy dissipating system would be an additional element in the form of foams. It follows from the numerical calculation results that a higher specific absorbed energy was obtained for the composite energy absorbing element with filler. The proposed method, based on numerical investigation, will allow for eliminating expensive and long-lasting testing of real objects. The obtained results will serve as guidelines to develop methods of testing for such structures and can be used in further research on increasing the security level in road transport.
W pracy rozważono problem związany z poprawą bezpieczeństwa transportu przez zastosowanie dodatkowych elementów absorbujących energię uderzenia. Przedstawiono wyniki badań eksperymentalnych oraz symulacji numerycznych podstawowego elementu energochłonnego w postaci tulejki wykonanej ze stali, duraluminium, mosiądzu i kompozytu szklano epoksydowego. Wyniki tych badań posłużą do zbudowania wiarygodnego modelu numerycznego panelu elementów ochronnych. Analizę numeryczną wykonano metodą elektów skończonych w oprogramowaniu DYTRAN. Przeprowadzone obliczenia zostały zweryfikowane eksperymentalnie na maszynie wytrzymałościowej INSTRON w Zakładzie Mechaniki Ogólnej WAT. W wyniku badań numerycznych i eksperymentalnych stwierdzono, iż tulejki kompozytowe mają dwukrotnie większą względną energię absorpcji niż tulejki stalowe. Interesującym jest uzupełnienie układu rozpraszającego energię o dodatkowy element w postaci pian. W wyniku obliczeń numerycznych stwierdzono, iż względną maksymalną energię odkształcenia uzyskano dla kompozytowego elementu energochłonnego z wypełniaczem. Proponowana metoda oparta na badaniach numerycznych pozwoli na wyeliminowanie kosztownych i długotrwałych badań rzeczywistych obiektów. Otrzymane wyniki posłużą jako wytyczne do opracowania metodyki badania tego typu struktur i będą mogły być wykorzystywane w dalszych pracach badawczych w zakresie zwiększenia poziomu bezpieczeństwa w transporcie drogowym.
Źródło:: Journal of KONES; 2007, 14, 1; 27-38
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 3.

Tytuł:: Analysis of influence of the shape of protective structures on their energy-absorbing capabilities
Analiza wpływu kształtu struktur ochronnych na ich energochłonność
Autorzy:: Barnat, W.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/241729.pdf
Data publikacji:: 2007
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: wpływ kształtu na energochłonność
impuls ciśnienia
energochłonność
influence of shape on energy-absorbing capability
pressure impulse
energy-absorbing capabilities
Opis:: The paper presents results of numerical investigation of the influence of the shape of a protective element on its energy-absorbing capabilities from the point of view of its resistance to the impact of a shock wave. The works carried out so far confirm that-- as far as the energy-absorbing capabilities are concerned - the shape of the protective element is an important factor. In the paper, results of numerical analysis of basic protective structures in the shape of pyramids, cones and hemispheres were presented. In the numerical models under consideration, dimensions of the base and height of the element were settled. The shape of the base determines the lateral surface of a cone. For the settled dimensions, a cone has the smallest area of the lateral surface and a sphere - the largest. For the models of basic structures, computations were performed with the use of the Dytran programme. As a result of the analysis, deformation of the structures, energy of deformation, velocities and accelerations were obtained. In the paper, a criterion for the assessment of energy absorption capabilities was proposed. It consisted in comparing the results for plates with a protection structure with those for a basic smooth plate in order to assess the level of energy absorbed by the protected plate with respect to the basic one (without protection).The comparison of results for the basic plate and the one with a spherical element shows that the application of the structure would cause the relative displacement of the plate protected a spherical element 50 percent lower than the relative displacement of the plate without protection.
W niniejszym artykule przedstawiono wyniki z przeprowadzonych badań numerycznych nad wpływem kształtu elementu ochronnego na energochłonność pod kątem odporności na działanie fali uderzeniowej. Dotychczasowe prace nad elementami energochłonnymi potwierdzają, iż dość ważnym z punktu widzenia energochłonności jest kształt elementu energochłonnego. W artykule przedstawiono wyniki z analizy numerycznej podstawowych struktur energochłonnych w postaci ostrosłupów stożków i półsfery. W modelach numerycznych ustalono wielkość podstawy oraz wysokość elementu struktury. Kształt podstawy determinuje pole powierzchni elementu. Najmniejsze pole powierzchni bocznej ma stożek. Największe pole powierzchni charakteryzuje sferę. Dla modeli struktur podstawowych wykonano obliczenia programem Dytran. W wyniku analizy numerycznej otrzymano postacie deformacji struktur, energię odkształcenia prędkości oraz przyspieszenia. W pracy przyjęto kryterium oceny energochłonności, polegające na porównaniu wyników płyt ze strukturą ochronną z płytą bazową gładką, w celu oceny zmiany poziomu energii pochłoniętej przez płytę zabezpieczoną w stosunku do płyty bazowej (bez zabezpieczenia). Porównanie wyników dla blachy bazowej i blachy z elementem sferycznym pokazuje, że zastosowane struktury powodowały względne przemieszczenie węzła płyty chronionej elementem sferycznym mniejsze o 50% od względnego przemieszczenia płyty.
Źródło:: Journal of KONES; 2007, 14, 1; 15-26
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 4.

Tytuł:: Numerical calculations of RVE dimensions for two-phase material
Autorzy:: Miedzińska, D.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/242298.pdf
Data publikacji:: 2011
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: microstructure
two-phase material
metal-ceramic composite
RVE
Opis:: A representative volume element (RVE) is a statistical representation of typical material properties. It should contain enough information on the microstructure thereby be sufficiently smaller than the macroscopic structural dimensions. The paper deals with the numerical calculations of the dimensions of the RVE for a two-phase material microstructure. Two and three dimensional models are taken into consideration. The structure of the samples are developed on the base of randomization of elements belonging to one of the phases. The phases volume share is 50/50%. The following series of the models are analyzed: from 10 x 10 to 100 x 100 elements for 2D samples and from 10 x 10 x 10 to 100 x 100 x 100 elements for 3D samples. The element characteristic dimension is 10 jm. The elastic behavior of the base materials (magnesium and alumina) is taken into account. The quasi-static compression tests of the developed structures are carried out with the use of LS-DYNA computer code. The results are presented as the equivalent Young modulus values and compared to the calculations based on the rule of mixtures. The stabilization of the achieved results allows to assess the dimensions of the RVE for two-phase material with random distribution.
Źródło:: Journal of KONES; 2011, 18, 2; 303-310
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 5.

Tytuł:: Numerical-experimental investigation of failure energy of composite energy absorbing panels
Numeryczno doświadczalne badanie energii zniszczenia podstawowych struktur kompozytowych
Autorzy:: Niezgoda, T.
Barnat, W.
Powiązania:: https://bibliotekanauki.pl/articles/242802.pdf
Data publikacji:: 2007
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: transport
elementy energochłonne
kompozyty
modele numeryczne
analiza numeryczna
energy absorbing elements
composites
numeric models
numerical analysis
Opis:: The aim of the paper is an assessment of the influence of the applied fill on the energy absorbing capabilities of a composite element of a thin-walled structure under dynamic load. The experimental tests were carried out on the INSTRON universal testing machine. The analysis concerned energy absorbing elements in a shape of sleeves with additional foam fill. The numeric model charge was made like in previously carried out experiments, using cinematic input function. Analysed models were charged by a rigid plate, described by a material MATRIG type. Foam filler use had for result the energy absorption improvement; this is important in the case of modernisation of existing structures using foam filler. An important advantage of energy absorbing elements made of composite materials is their little mass. In the case of considering of protection elements for aviation industry, this factor is very important. The presented results are preliminary tests of energy absorbing filler choice and will be applied for numeric models validation. The conclusion of preliminary estimation of obtained elements is that the appropriate choice of filler material will permit to obtain more important energy necessary for destruction of energy absorbing structure. The future application of numeric analyse will facilitate the process of filler parameters optimisation.
Źródło:: Journal of KONES; 2007, 14, 4; 307-318
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 6.

Tytuł:: Numerical analysis of progressive failure of composite energy absorbing structures
Autorzy:: Niezgoda, T.
Barnat, W.
Powiązania:: https://bibliotekanauki.pl/articles/243301.pdf
Data publikacji:: 2008
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: transport safety
road barriers
numerical analysis
energy-absorbing element
FEM
Opis:: The aim of the paper was to compare the influence of the applied fill on the energy absorbed by the energy ubsorbing structural elements made of composite, steel and from composite with fill foam. The experimental tests were carried out on an INSTRON universal testing machine at the speed rate of the machine's traverse equal 10 mm/min md the numerical analysis has been performed using MSC. Dytran software based on the Finite Element Method. The elements were subjected to axial kinematic loads. The higher specific absorbed energy occurs in the case of energy absorbing elements made of composites and from composite with fill foam. These elements can be applied in structures designed for the protection of people or limitation of the whole structure failure, e.g. in the case of a helicopter or car crash etc. The failure progressing in a relatively uniform manner results in the fact that the work md for failure of an energy absorbing element causes a substantial reduction of the impact load results. Application of energy absorbing elements may be a system dissipating the energy of a car impact into a crash barrier. The results of numerical simulation of stiffness plate hitting to the road barrier are presented. Experimental tests and numerical simulations were also presented for a composite sleeve subjected to progressive failure, which allowed carrying out simulation and analysis of a crash into a road barrier protected by a system of two such sleeves.
Źródło:: Journal of KONES; 2008, 15, 1; 169-181
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 7.

Tytuł:: Numerical study of the projectile trajectory disturbing during the oblique impacts
Autorzy:: Morka, A.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/244096.pdf
Data publikacji:: 2010
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: computational mechanics
impact problem
armour perforation
ballistic resistance
oblique impact
Opis:: The numerical investigations have been performed to determine the effect of the projectile trajectory disturbing during oblique impacts. An impact of the 14.5x118 mm B32 armour piercing projectile on the A12O3 different shape elements backed by 7017 aluminum alloy plate was analyzed. The oblique impact was realized by different shapes of the frontal ceramic elements, including hemispheres and pyramids, with respect to standard flat tiles. The influence of the impact point location was also under considerations. The Computer simulations were performed with the Element Free Galerkin Method (EFG) implemented in LS-DYNA code. full 3D models of the projectile and targets were developed with strain rate and temperature dependent material constitutive relations. The Johson-Cook model was applied to describe the metallic parts, while the ceramic was modelled by Johnson-Holmquist constitutive relations. The models of the projectile, ceramic and aluminium alloy targets were validated with utilization of the experimental datafound in literature. The obtained results confirmed that the projectile trajectory undergoes essential deviation because of the projectile angular velocity. The conditions for maximizing the value of this angular velocity were studied and it is possible to reach several radians per millisecond. The conclusions presented in this paper can be applied to develop modern impact protection panels where the appropriate balance between the mass and protection level must be accomplished.
Źródło:: Journal of KONES; 2010, 17, 3; 307-312
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 8.

Tytuł:: Thermomechanical FE analysis of the engine piston made of composite material with low histeresis
Autorzy:: Szurgott, P.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/244407.pdf
Data publikacji:: 2011
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: engine piston
composite piston
coefficient of thermal expansion
thermal analysis
FE analysis
Opis:: The main purpose of the preliminary analyses presented in the paper was to compare the behaviour of the combustion engine piston made of different type of materials under thermal load. A thermomechanical FE analysis of the engine piston made of composite material was shown. A selected engine is installed in one of the popular polish tanks. The proposed new material is characterized by a low hysteresis – the differences of the coefficient of thermal expansion for heating and cooling are not significant. The results obtained for the piston made of a new material were compared with those for the current standard material. The piston was loaded by a temperature field inside it. Appropriate averaged thermal boundary conditions such as temperatures and heat fluxes were set on different surfaces of the FE model. FE analyses were carried out using MSC.Marc software. Development of the FE model was also presented. Geometrical CAD model of the piston was developed based on the actual engine piston, which was scanned using a 3D laser scanner. A cloud of points obtained from the scanner was processed and converted into a 3- dimensional solid model. FE model of a quarter part of the piston was developed for the preliminary analysis presented in the paper. 4-node tetrahedron finite elements were applied since there was no axial symmetry of the considered object. The temperature field inside the piston was determined and presented in the form of contour bands. Contours of displacement and stress in a radial direction were shown as well.
Źródło:: Journal of KONES; 2011, 18, 1; 645-650
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 9.

Tytuł:: CI engine as a case study of thermomechanical FE analysis of the piston - piston rings - cylinder system
Autorzy:: Szurgott, P.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/247997.pdf
Data publikacji:: 2012
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: engine piston
composite piston
thermomechanical analysis
FE analysis
Opis:: The compression-ignition engine as a case study of a methodology of the numerical modelling and simulation of the piston - piston rings - cylinder system was presented in the paper. Thermomechanical FE analysis, taking into account thermal and mechanical loads, was carried out using the MSC.Marc/Mentat software. The mechanical loads included loads due to inertial and gas forces as well. A three dimensional solid geometrical model of the considered set was developed using AutoCAD software, whereas the finite element mesh was generated using Altair HyperMesh. Kinematic boundary conditions - the vertical displacement and acceleration of the piston - were described by the corresponding curves as a function of time for selected engine speed. Changes in pressure on the piston crown were estimated based on data from the engine manufacturer and the corresponded indicator diagram available in the literature. The results of thermomechanical FE analysis were presented in the form of stress and/or displacement contours. The main aim of the analysis was to determine the deformation of the piston depending of on the piston material. Two types of material were compared - the actual one PA12 aluminum alloy and the new composite material with low hysteresis. The second material was characterized by slight differences of the coefficient of thermal expansion for heating and cooling.
Źródło:: Journal of KONES; 2012, 19, 1; 399-406
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 10.

Tytuł:: Numerical study of the shape effect in the ceramic based ballistic panels
Autorzy:: Morka, A.
Jackowska, B.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/245901.pdf
Data publikacji:: 2009
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: computational mechanics
impact problem
armour perforation
ballistic resistance
ceramic armour
Opis:: The numerical investigations have been performed to determine the front surface shape effect in the cer based armour systems. Different shapes of ceramic elements were analyzed, including hemispheres and pyramids with respect to standard flat tiles. The influence of the impact point location was also under considerations. The Computer simulations were performed with the Element Free Galerkin Method (EFG) implemented in LS-D code. An impact of the 14.5xll8mm B32 armour piercing projectile on the A12O3 different shape elements backe 7017 aluminium alloy plate was analyzed. Full 3D models of the projectile and targets were developed with strain, rate and temperature dependent material constitutive relations. The models of the projectile, ceramic and aluminium alloy targets were validated with utilization of the experimental data found in literature. The obtained results confirm, the preliminary presumptions, that the shape of the front surface can significant role in the overall ballistic resistance of the panel. Particularly projectile-target initial contact area st to be important factor as showed by impact point location analysis. The conclusions presented in this paper can be applied to develop modern impact protection panels where the appropriate balance between the mass and protection level must be accomplished.
Źródło:: Journal of KONES; 2009, 16, 4; 539-548
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 11.

Tytuł:: Investigation of human body exposed to blast wave derived from improvised explosive devices
Autorzy:: Sławiński, G.
Dziewulski, P.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/246647.pdf
Data publikacji:: 2015
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: vehicle safety
mine resistance
improvised explosive device
occupant safety
FEM analysis
Opis:: The analysis of contemporary military conflicts shows, that the most dangerous threat for soldiers are Improvised Explosive Devices (IEDs). Blast resistance of military vehicles and structures is broadly discussed in many articles. However, information about human body response to impact loading is hard to find and very general. Both experi-mental trials with dummies and numerical analyses are needed. To design and develop better protection system it is necessary to identify and measure the effects of blast wave impact on crew of military vehicle. This paper presents numerical simulation results of special armoured vehicle subjected to mine threat of 8 and 10 kg of TNT. Possible effects of mine explosion on human body are described. Review of modern-mine and IED countermeasure solutions is presented. The analysis is conducted using LS-DYNA explicit code. Only vehicle’s hull is considered with suspension and turret is modelled using mass. Gravity is taken into account. Numerical model of Hybrid-III dummy is used. Accelerations and forces in tibia, neck and spine were calculated. HIC-36 criterion was also evaluated Different types of possible seat configuration are examined. Results show convergence between explosive size and injury risk.
Źródło:: Journal of KONES; 2015, 22, 4; 287-294
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 12.

Tytuł:: New method of carbon dioxide underground storage coupled with shale gas recovery
Autorzy:: Niezgoda, T.
Miedzińska, D.
Kędzierski, P.
Powiązania:: https://bibliotekanauki.pl/articles/246774.pdf
Data publikacji:: 2012
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: shale gas
carbon dioxide
storage system
Opis:: Shale gas is natural gas produced from shale, a type of sedimentary rock. Shale gas has become an increasingly important source of natural gas in the United States over the past decade, and interest has spread to potential gas shales in Canada, Europe, Asia, and Australia. One analyst expects shale gas to supply as much as half the natural gas production in North America by 2020. As of 2010, Poland imports two-thirds of its natural gas from Russia. ConocoPhillips has announced plans to explore for shale gas in Poland, along with Lane energy. The recently made available US Department of Energy report revealed that the largest reserves of shale gas in Europe are in Poland. The authors of the report calculate that Poland has reserves of about 22.45 trillion cubic meters of shale gas, of which 5.30 trillion cubic meters is immediately available for extracting. The most common method of shale gas recovery is hydraulic fracturing - the propagation of fractures in a rock layer caused by the presence of a pressurized fluid. Hydraulic fractures form naturally, as in the case of veins or dikes, and is one means by which gas and petroleum from source rocks may migrate to reservoir rocks. This process is used to release petroleum, natural gas (including shale gas, tight gas and coal seam gas), or other substances for extraction, via a technique called induced hydraulic fracturing. The method is critically assessed by ecologists. The paper deals with new method of gas shale fracturing and gas recovery coupled with carbon dioxide storage. It allows to effectively mine the shale gas and to store carbon dioxide in shale rock. It must be noticed that CO2 pollution is a very important problem in Poland, because of European Union CO2 limits. Also the numerical calculation of carbon dioxide thermodynamical process of decompression process, which simulates the injection of the cold liquid gas into the shale formation (high temperature and pressure conditions) and its influence on shale rock fracturing will be presented.
Źródło:: Journal of KONES; 2012, 19, 3; 327-333
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 13.

Tytuł:: Analysis of a light caterpillar vehicle loaded with blast wave from detonated IED
Autorzy:: Barnat, W.
Niezgoda, T.
Panowicz, R.
Powiązania:: https://bibliotekanauki.pl/articles/247638.pdf
Data publikacji:: 2010
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: IED
vehicle shell
FE analysis
ground
Opis:: More and more impudent attacks on the military convoys in Afghanistan proved a huge danger of the improvised explosive devices - IED. Huger and more clever charges are a serious problem for vehicles protection. Additionally, hitherto defence standards and STANAG didn't predict such huge charges. Majority investigations were based on a 3 kg anti-tank mine. The article presents the results of numerical calculations for the elements of the combat vehicle supporting structure loaded with an impact generated by explosion of a huge explosive charge under the bottom of the vehicle with consideration of the wave reflected from the ground. Such an approach allows obtaining a good approximation of numerical simulations to real conditions of terroristic attacks. Additionally, the analysis of IED side influence on the vehicle shell was conducted. The explosive charge — IED — was simulated with the use of concentrated energy of properly selected (on the base of literature investigations) density and initial energy. During analyses of side explosive on the vehicle structure, the obstacle in the form of a building increasing the pressure impulse was taken into account. The paper presents the results of a numerical analysis in which Euler and Lagrange domains(describing a vehicle) were coupled. A perfect gas model was used to describe air parameters.. Additionally, the ground was described with a gas model. Every kind of material data were selected on the base of experimental investigations. A bilinear material model with a Cowper and Symonds strain rate model was used to describe a vehicle. Such an approach fully describes the phenomena occurring in the system.
Źródło:: Journal of KONES; 2010, 17, 4; 27-34
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 14.

Tytuł:: Numerical model of bullet - barrel system
Model numeryczny układu lufa - pocisk
Autorzy:: Łazowski, J.
Małachowski, J.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/241651.pdf
Data publikacji:: 2007
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: lufa
pocisk
modelowanie numeryczne
barrel
bullet
numerical modelling
Opis:: Aktualnie, projektowanie uzbrojenia w dużej mierze opiera się na metodach analitycznych, które nie pozwalają na znaczną poprawę parametrów broni w zakresie odporności udarowej. Szczególnie istotna jest analiza dynamiki dla ruchu pocisku w lufie na stożku przejściowym i ustalenie optymalnych parametrów procesu. Na styku lufy i pocisku zachodzą bardzo złożone procesy termomechaniczne. Oddziaływanie to powoduje powstawanie na powierzchni styku ciał ciepła a w konsekwencji zmian właściwości mechanicznych. Dodatkowo charakter współpracy obu ciał obarczony jest często brakiem symetrii wynikającym między innymi z niedokładności wykonania elementów, nieodpowiednim osadzeniem pocisku w lufie oraz niejednorodnością materiałów. W skutek takiej złożoności zjawisk, której konsekwencją są np. zmienność współczynnika tarcia czy również drgania pocisku i lufy, ogólne analityczne wyznaczanie stanów naprężeń i stanów krytycznych w sposób ścisły jest niemożliwe. Jedyną skuteczną metodą może być w tym przypadku modelowanie numeryczne. W pracy przedstawiono próbę analizy stanu wytężenia powstającego podczas szybkozmiennych procesów w trakcie współpracy pocisku z lufą. Przedstawiono model numeryczny obiektów i zaprezentowano wyniki analizy w formie planów warstwicowych. Narzędziem zastosowanym do analizy był pakiet obliczeniowy LS-DYNA umożliwiający symulacje w zakresie nieliniowym z jawnym krokiem całkowania.
Currently the design process for armament equipment mostly employs very known and traditional analytical methods. But in many cases this kind of approach is not sufficient and effective, especially for gun parameters related with impact resistance. Very crucial for proper dynamic bullet movement in the barrel are geometric dimensions. In the contact areas between a bullet and a barrel appear some thermo-mechanical phenomena. Additionally, the cooperation process between these two components is encumbered because of the asymmetry caused by the inaccuracy of production process and the inhomogeneity of used materials. Finally, the mentioned reasons produce some unwanted effects like: bullet and barrel vibrations, problems with friction phenomena, etc. In such situations, the typical engineering approach in design process is unable to take into considerations all such local and very complex effects. Therefore, this paper presents is a trial of numerical methods application, which allow perform full analysis process of interaction between bullet and barrel. The models of these two bodies were developed using FE method. The numerical calculations were performed using LS-DYNA code. The main goal of the research was focused on contact problem. In the paper authors enclosed the initial results of the dynamic simulations.
Źródło:: Journal of KONES; 2007, 14, 1; 261-266
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Tytuł:: Preliminary concept of numerical modelling of combustion process for gunpowder using LS-DYNA code
Wstępna koncepcja numerycznego modelowania procesu spalania ładunku miotającego w systemie LS-DYNA
Autorzy:: Łazowski, J.
Małachowski, J.
Niezgoda, T.
Powiązania:: https://bibliotekanauki.pl/articles/241653.pdf
Data publikacji:: 2007
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: lufa
pocisk
modelowanie numeryczne
balistyka wewnętrzna
spalanie
barrel
bullet
numerical modelling
internal ballistic
gunpowder burning
Opis:: In this paper the preliminary concept of numerical modelling of combustion process for gunpowder is presented. Such new computational methods like finite element analysis gave us opportunity to simulate such energetic and high-frequency process like pressure wave generation caused by chemical reaction. The main product of this process is a blast wave, which interacts at the first stage with surrounding (bullet and shell) and finally impel a bullet movement. In the considered case, the detonation product from gunpowder burning couple "produced" gas in Eulerian domain with the barrel-bullet system described in Lagrangian domain. In the performed analysis, the authors noticed some unwanted effects like asymmetry, which is probably related with the finite element mesh and computational errors. In the next conducting investigations some optimisation procedures related with a bullet movement in a barrel will be employed. The successful solution of such complicated problem like a proper simulation of the internal ballistic phenomena with taking into account all dynamic effects can significantly improve the problem of shooting accuracy. The initial calculations were performed using LS-Dyna code. At this stage the presented results have a qualitative character.
W pracy omówiono koncepcję symulacji komputerowej spalania materiału wybuchowego miotającego w układzie lufa- nabój. Takie nowoczesne sposoby obliczeniowe, oparte na metodzie elementów skończonych mogą dostarczyć możliwości symulacji szybkozmiennych procesów energetycznych wynikających ze zamiany energii chemicznej prochu na ciśnienie gazów prochowych i w konsekwencji w energię kinetyczną pocisku. Okazuje się, że zamodelowanie wytwarzania produktów spalania materiału miotającego jest zadaniem trudnym. W takich ekstremalnych warunkach charakter współpracy obu ciał może być obarczony np. brakiem symetrii wynikającym między innymi z asymetrycznego rozkładu ciśnienia produktów spalania materiałów miotających. W przypadku modelu dyskretnego koncepcja ta może zostać wykorzystana do rozwiązania problemu głównego balistyki wewnętrznej i optymalizacji konstrukcji układu lufa - nabój oraz symulacji właściwości dynamicznych rozpatrywanych obiektów w różnych fazach współpracy. Poniżej przedstawiono klasyczne sformowanie modelu dla broni lufowej oparte równań matematycznych i sposób zaimplementowania w modelu dyskretnym. Rozważania zilustrowano przykładowymi wynikami. Pracę realizowano przy wykorzystaniu licencjonowanego pakietu obliczeniowego LS-Dyna. Przedstawione wstępne wyniki mają charakter jakościowy.
Źródło:: Journal of KONES; 2007, 14, 1; 255-260
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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