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Tytuł:
Numerical study of tires behaviour
Numeryczne testowanie opon
Autorzy:
Małachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/246419.pdf
Data publikacji:
2007
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
opona
modelowanie
metoda elementów skończonych
testy dynamiczne
tire
modelling
finite element method (FEM)
dynamic tests
Opis:
Głównym celem referatu jest przedstawienie problematyki modelowania opon (kół) jako elementów konstrukcji pojazdów. W pracy pokazane są różne przykłady modelowania tych konstrukcji na przykładzie koła samochodu ciężarowego, koła podwozia samolotu transportowego oraz koła samochodu osobowego. W każdym z tych trzech przypadków przedstawiono trzy różne techniki modelowania, od najprostszego modelu dla pojazdu ciężarowego, aż do najbardziej skomplikowanego modelu koła w przypadku pojazdu osobowego. Wykorzystanie zaawansowanych systemów CAD/CAE pozwoliło na stworzenie w szybkim czasie złożonego modelu koła samochodu osobowego, który stał się bazą do obliczeń numerycznych z zastosowaniem metody elementów skończonych. Przy tworzeniu modelu numerycznego koła położono nacisk na zamodelowanie wewnętrznych części składowych (opasanie, osnowa, drutówka). Jednak szczególną uwagę zwrócono na dokładne odwzorowanie bieżnika. Udało się to dzięki zastosowaniu nowoczesnej techniki ,,reverse engineering". Obliczenia we wszystkich trzech przypadkach przeprowadzono z wykorzystaniem jawnej procedury całkowania zawartej w systemie LS-Dyna.
The main aim of this research was focused on FE tires model development. To reach this goal the real tires were scanned using digitising arm and than transferred to CAD software. The total FE models were created in the MSC.Patran software. The applied technique is called reverse engineering. In this models major wheel elements like belt, tread, side wall, drum and rim were included. In order to realistically simulate the interaction between the tire and surface, internal pressure is appropriately represented by applying airbag option to the wheel model. In such situations the volume is defined as the volume enclosed by a surface. In analysed cases the control volume were modelled by shell elements comprising the airbag fabric material. The area of the control surface which surrounds analysed volume is related to the control volume according to Greens 's theory. To describe other rubber components of the tyre, such as a tyre tread and tyre sides, a material model of rubber was applied. Due to the complex and irregular shape of the tire (tread, rim, side wall) it was decided to use structural elements such solid elements. Numerical analysis was performed using LS-Dyna code. Finally, some results from performed tests are enclosed in this paper.
Źródło:
Journal of KONES; 2007, 14, 3; 377-384
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Computational studies of gas pipeline junction in unusual operating scenario
Autorzy:
Małachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/242257.pdf
Data publikacji:
2009
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
security
numerical simulations
explosive material
pipeline junction
Opis:
This research has been inspired by security concerns due to the recent increase in the terrorist threat to gas and crude oil transportation around the world, especially in regions that are of significant value for the energy supplies. Computational mechanics methods will be used in this research to apply shock wave analysis for possible damage assessment of the affected pipelines. These methods may be also used for pipelines at power plants, which are usually placed high on the homeland security priority list. The main goal of this research is focused on establishing effective simulation methodology to study the influence of shock waves (caused by explosion) on pipeline infrastructure elements placed on surface to ensure their security. This study is primarily focused on the behaviour of some type of pipeline junction existing in gas pipeline system which can be subjected to the shock wave produced by the detonation ofhighly explosive (HE) materials. Outcomes of this research are important in preventing damage progression of pipelines under the blast loading. This data will also be used to develop improved design guidelines for safer and less vulnerable pipelines.
Źródło:
Journal of KONES; 2009, 16, 2; 299-304
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Blast wave and suspension system interaction - numerical approach
Autorzy:
Baranowski, P.
Małachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/247125.pdf
Data publikacji:
2011
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
suspension system
pressure wave
SPH
ALE
FE modeling
Opis:
The main aim of this paper is to present the effective example of coupled experimental and numerical tests. Moreover, a development process of a numerical model of a terrain vehicle suspension system is presented. Experimental tests were carried out on the machine Instron 8802 with an assistance of the high-speed camera Phantom v12. Obtained stress-strain curves were applied into the FE model to estimate material constants for Mooney-Rivlin constitutive rubber model and for numerical failure criterion. Geometry of the tire and other suspension elements were achieved using reverse engineering technology. Due to the fact that a tire is such a complex structure to be represented with numerical methods, it was important to develop a discrete model of tire as much similar to the real one as possible. Consequently, an exact tire cords pattern was implemented into the FE model of the tire, which was obtained by the assistance of a microscope and X-ray device. In the next step, numerical analyses were performed simulating the TNT explosion under the suspension system with a simplified motor-car body. Nonlinear dynamic simulations were carried out using the explicit LS-Dyna code, with central difference scheme with modified the time integration of the equation of motion. In order to simulate the blast wave propagation the Smoothed Particle Hydrodynamics (SPH) method and Arbitrary Lagrangian-Eulerian formulation with Jones Wilkins Lee (JWL) equation defining the explosive material were used. Finally, results from both approaches were compared.
Źródło:
Journal of KONES; 2011, 18, 2; 17-24
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Dynamics analysis of the main landing gear in 3D model
Analiza dynamiczna podwozia głównego w modelu 3D
Autorzy:
Krasoń, W.
Małachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/247885.pdf
Data publikacji:
2007
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
podwozie samolotowe
modelowanie numeryczne
zrzutowy test lądowania
MES (metoda elementów skończonych)
aircraft landing gear
numerical modelling
touchdown drop test
FEM
Opis:
Właściwie dobrane charakterystyki podwozia pozwalają minimalizować obciążenia występujące w podzespołach układu podwozia podczas jego pracy w momencie przyziemienia. W związku z tym wykonuje się analizy dynamiczne podwozi, aby przewidzieć ich zachowanie się w warunkach dla nich niebezpiecznych. Przeprowadzenie tego typu badań z wykorzystaniem metod numerycznych jest znacznie łatwiejsze i tańsze od prób stanowiskowych. W pracy omawiana jest metodyka modelowania podwozia głównego i procedury doboru parametrów opisujących rzeczywistą strukturę badanego układu. W celu określenia właściwości materiałowych elementów składowych układu podwozia definiowane są sprężyste i nieliniowe charakterystyki materiałowe. W modelu numerycznym MES uwzględniono następujące zagadnienia: kontakt pomiędzy współpracującymi częściami układu, zjawisko pochłaniania energii w amortyzatorze gazowo-cieczowym zastosowanym w podwoziu, oddziaływanie gruntu na odkształcalną oponę podczas przyziemienia. Wybrane wyniki analizy numerycznej odpowiadające przypadkowi maksymalnych obciążeń podwozia podczas przyziemienia na 3 punkty z maksymalną dopuszczalną prędkością pionową będą omawiane wraz z wynikami testów stanowiskowych. Prezentowana w pracy analiza jest pierwszą częścią badań numerycznych trwałości podwozia lotniczego.
Properly adjusted characteristics enable minimisation of loads that occur in the landing-gear components at the moment of touchdown. Therefore, dynamic analyses of the landing gear are conducted to provide capabilities to forecast their behaviour under hazardous conditions. This kind of investigation with numerical methods applied is much easier and less expensive than stand tests. However, the development of the landing gear FEM models is necessary. Methodology of the main landing gear numerical models developing and procedures of parameters selection for the real structure features representation is discussed in the paper. The nonlinear physical material properties were precisely defined. To describe material properties of all mechanical components of the landing gear, a materials chart describing parameters for the elastic range was used. In FEM model the following matters were taken into consideration: contact problems between collaborating elements, the phenomena of energy absorption by gas-liquid damper placed in the landing gear and the response of the landing gear during touchdown of a flexible wheel with the ground. Chosen results of the numerical analysis for the maximum load of the gear considered, corresponding to an aircraft's 3-point landing at maximum decline speed allowed have been compared to experimental research's results. The analysis presented in this paper is the first part of wider considerations concerning numerical assessment of landing gear life.
Źródło:
Journal of KONES; 2007, 14, 3; 305-310
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Numerical investigations of terrain vehicle tire subjected to blast wave
Autorzy:
Baranowski, P.
Małachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/243723.pdf
Data publikacji:
2011
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
blast wave
finite element analysis
SPH
JWL
tire
vehicle suspension system
vehicle suspension
Opis:
In this paper a numerical model of a terrain vehicle suspension system development process is presented. In the performed studies the suspension system with and without a simplified motor-car body was taken into consideration. Geometry of the tire, wheel and system elements were achieved using reverse engineering technology. Moreover, with the assistance of a microscope and an X-ray device it was possible to achieve the exact tire cords pattern, which in the next stages was implemented into the FE model. Subsequently, numerical simulations of both cases were performed simulating the TNT explosion under a wheel. The non-linear dynamic analyses were performed using the LS-DYNA code. To solve both presented cases the explicit central difference scheme with modified time integration of the equation of motion was implemented. Computations of blast wave propagation were carried out with the Smooth Particle Hydrodynamics (SPH) method with Jones Wilkins Lee (JWL) equation of state defining the explosive material. Obtained results have shown different suspension system elements damage and tire destruction characteristic, which come from blast wave reflection of the motor-car body surface.
Źródło:
Journal of KONES; 2011, 18, 1; 23-30
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Numerical study of selected military vehicle chassis subjected to blast loading in terms of tire strength improving
Autorzy:
Baranowski, P.
Malachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/199788.pdf
Data publikacji:
2015
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
blast loading
LAV
tire
FE analysis
opona
analiza MES
Opis:
In the paper a chosen model of the light armoured vehicle was tested in terms of blast loading. More precisely, the blast propagation and interaction with the tire behaviour and suspension system elements of the light-armoured vehicle (LAV) was simulated. The chosen military vehicle meets the requirements of levels 2A and 2B of STANAG 4569 standard. Based on the obtained results, two modifications were proposed for the strength and resistance improvement of the wheel. The first consisted of inserting the rubber runflat ring inside the tire, whereas in the second the honeycomb-like composite wheel was implemented. Non-linear dynamic simulations were carried out using the explicit LS-Dyna code, with multi-material Arbitrary Lagrangian-Eulerian formulation for simulation the blast process.
Źródło:
Bulletin of the Polish Academy of Sciences. Technical Sciences; 2015, 63, 4; 867-878
0239-7528
Pojawia się w:
Bulletin of the Polish Academy of Sciences. Technical Sciences
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Multibody rigid models and 3D FE models in numerical analysis of transport aircraft main landing gear
Autorzy:
Krason, W.
Malachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/200211.pdf
Data publikacji:
2015
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
transport aircraft
main landing gear
numerical tests
rigid and 3D FE models
samolot transportowy
podwozie główne
metodologia testów numerycznych
Opis:
Dynamic analyses of a transport aircraft landing gear are conducted to determine the effort of such a complex system and provide capabilities to predict their behaviour under hazardous conditions. This kind of investigation with the use of numerical methods implementation is much easier and less expensive than stand tests. Various 3D models of the landing gear part are defined for the multistage static FE analysis. A complete system of the main landing gear was mapped as a deformable 3D numerical model for dynamic analysis with the use of LS-Dyna code. In this 3D deformable FE model, developed in a drop test simulation, the following matters were taken into consideration: contact problems between collaborating elements, the phenomena of energy absorption by a gas-liquid damper placed in the landing gear and the response of the landing gear during the touchdown of a flexible wheel with the ground. The results of numerical analyses for the selected drop tests and the results from the experiments carried out on a real landing gear were used for verification of FE models and a methodology of the landing gear dynamics analysis. The results obtained from the various simulations of the touchdown have proved the effectiveness of the 3D numerical model and how many problems can be solved in the course of only one numerical run, e.g. geometric and material nonlinearities, a question of contact between the mating components, investigation of the landing gear kinematics, investigation of the energy dissipation problem in the whole system and the stresses influence on the structure behaviour, which can appear in some elements due to overload.
Źródło:
Bulletin of the Polish Academy of Sciences. Technical Sciences; 2015, 63, 3; 745-757
0239-7528
Pojawia się w:
Bulletin of the Polish Academy of Sciences. Technical Sciences
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Numeryczna analiza wytężenia podwozia głównego z uszkodzeniem w dynamicznym teście przyziemienia
Numerical analysis of landing gear effort with failure in dynamic touchdown test
Autorzy:
Krasoń, W.
Małachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/208825.pdf
Data publikacji:
2010
Wydawca:
Wojskowa Akademia Techniczna im. Jarosława Dąbrowskiego
Tematy:
podwozie lotnicze
idealny/nominalny model MES i model 3D z uszkodzeniem
numeryczna symulacja przyziemienia
landing gear
ideal/nominal FE model and 3D model with failure
numerical simulation of touchdown test
Opis:
Lądowanie jest najniebezpieczniejszą fazą lotu samolotu. Głównym zadaniem podwozi lotniczych jest pochłanianie energii samolotu podczas lądowania i startu. Dlatego podwozie lotnicze musi posiadać odpowiednią wytrzymałość zapewniającą bezpieczeństwo i założony czas eksploatacji. Większość analiz zmęczeniowych i numerycznego prognozowania czasu eksploatacji podwozi lotniczych ogranicza się do liniowych analiz i badania zjawisk lokalnych występujących wokół uszkodzenia. Największą zaletą prezentowanej w pracy metody numerycznej jest możliwość zastosowania do badania kompletnego układu podwozia lotniczego z możliwością uwzględnienia uszkodzenia. Jest to niemożliwe do zrealizowania innymi metodami, w tym także za pomocą badań eksperymentalnych. W pracy przedstawiono idealny model MES oraz model podwozia z uwzględnieniem uszkodzenia. Modele takie zastosowano w analizie wytężenia poszczególnych podzespołów podwozia podczas różnych symulacji przyziemienia.
Landing is the most dangerous phase of aircraft flight. The primary purpose of the landing gear units is to absorb the impact energy of the aircraft when it lands and takes off. Therefore the landing gear has to sustain appropriate strength to guarantee safety and fatigue life. Majority of the fatigue numerical analysis and prediction of the landing gear's lifetime is limited to linear analysis and local phenomena appearing around a failure. The major advantage of the presented here numerical method is applicability there of to complete landing gear testing with artificially introduced flaws, what is impossible to be performed with other methods, including experimental testing work. The ideal FE model and the model with failure of the complete landing gear were studied in the paper to define the effort of particular components of the complete structure during various touchdown simulations.
Źródło:
Biuletyn Wojskowej Akademii Technicznej; 2010, 59, 1; 115-130
1234-5865
Pojawia się w:
Biuletyn Wojskowej Akademii Technicznej
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Badanie wpływu sformułowania elementu skończonego oraz schematu rozwiązywania równania ruchu na wyniki analizy MES na przykładzie niesymetrycznie obciążonej płyty
Study on the influence of finite element formulation and equation of motion solution scheme on FEM analysis results based on the asymmetrically loaded plate problem
Autorzy:
Krzeszowiec, M.
Małachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/210703.pdf
Data publikacji:
2015
Wydawca:
Wojskowa Akademia Techniczna im. Jarosława Dąbrowskiego
Tematy:
mechanika
metoda elementów skończonych
elementy powłokowe
całkowanie numeryczne równań ruchu
computational mechanics
finite element method
shell elements
numerical integration
Opis:
Komputerowe metody symulacji zjawisk fizycznych obecnie są powszechne zarówno w obszarze nauki, jak i przemysłu. Możliwość przybliżonego rozwiązywania skomplikowanych układów równań różniczkowych, opisujących zagadnienia z dziedziny mechaniki, fizyki czy chemii, pozwala na znaczne skrócenie czasu projektowania i wdrażania nowych projektów. Często dzieje się to przy jednoczesnym zmniejszeniu zapotrzebowania na kosztowne badania eksperymentalne lub wytwarzanie prototypów. Jednak wspomniana powszechność tych metod, w szczególności metody elementów skończonych, spowodowała, że symulacje oraz analizy przeprowadzane z ich wykorzystaniem są często z góry za dokładne. Celem tego artykułu jest przedstawienie na przykładzie prostej analizy wytrzymałościowej, jak duży wpływ na wyniki symulacji mają takie parametry jak gęstość siatki elementów skończonych, sformułowanie elementu skończonego czy schemat całkowania równania ruchu. Dodatkowo autorzy zdecydowali się pokazać, jak łatwo jest uzyskać wyniki, które nie przedstawiają sensu fizycznego, pomimo tego, że wszystkie podstawowe założenia poprawnej analizy (odpowiednie warunki brzegowe, zachowana energia układu etc.) zostały spełnione. Wyniki przeprowadzonych badań mogą być przestrogą przed pochopnym wyciąganiem wniosków z obliczeń przeprowadzonych za pomocą MES.
Computer simulations of physical phenomena are at the moment common both in science and industry. The possibility of finding approximate solutions for complicated systems of differential equations, mathematically describing issues in the fields of mechanics, physics or chemistry, allows for shorten design and research time, often significantly reducing the need for expensive experimental studies or costly production of prototypes. However, the mentioned prevalence of these methods, particularly the Finite Element Method, resulted in analysis outcomes to be often in advance regarded as accurate ones. The purpose of the article is to showcase, on a simple stress analysis problem, how parameters such as the density of the finite element mesh, finite element formulation or integration scheme significantly influence on the simulation results and how easy it is to end up with the results that do not hold any physical sense, despite the fact that all the basic assumptions of correct analysis (suitable boundary conditions, total system energy stored etc.) have been met. The results of this study can serve as a warning against premature conclusion drawing from calculations carried out by means of FEM simulation.
Źródło:
Biuletyn Wojskowej Akademii Technicznej; 2015, 64, 1; 139-159
1234-5865
Pojawia się w:
Biuletyn Wojskowej Akademii Technicznej
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Some selected FEM analyses of motion of a bullet with imperfections while interacting with the barrel
Autorzy:
Łazowski, J.
Małachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/243313.pdf
Data publikacji:
2008
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
barrel
bullet
simulation
movement modelling
imperfection
Opis:
The intended aim of studies on the modelling of a bullet interacting with a barrel is to generale a virtual, computer-based model, experimentally verified for some selected mating conditions, and to become able to predict -with strong probability - processes and phenomena that take place within a system with imperfections. In the case under consideration the problem of contact between the barrel and the bullet has been described with the calculation method based on the penalty function. Calculations were made using the so-called direct-integration procedurę, colloquially called the ,,explicit integration ". Preliminary analysis has been carried out on the effect of the shift of the centre ofmass of the bullet moving in the barrel. Simulation included the bullet displacement along the barrel's axis, with the assumed positions of the centre ofmass -5% and +5% as measured from the bottom and referred to the initial model (0%). Results ofnumerical calculations suggest the effect of shift of the bullet's centre of mass, which -when exposed to complex states of loading - experiences oscillating movements of the bottom and the tip. Additionally, this analysis proves that there is a complex state of stress due to compression, torsion, and bending of the bullet while interacting with the inner part of the barrel. Numerical solutions may support the analytically approached solving of such mechanical system. They may also offer more precise determination of, e.g. initial and boundary conditions for the bullet 's free flight, which is of great significance to the accuracy of fire, and therefore, to the weapons effectiveness.
Źródło:
Journal of KONES; 2008, 15, 1; 145-152
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
I-beam structure under blast loading-Eulerian mesh density study
Autorzy:
Mazurkiewicz, Ł.
Małachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/245483.pdf
Data publikacji:
2011
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
blast wave
FEM
Eulerian mesh
Opis:
Dynamic response of an I-beam structure subjected to shock wave produced by the detonation of high explosive (HE) materials is presented in this paper. LS-DYNA, a 3-D explicit, finite element computer code is used to study this behaviour. A coupled analysis between Lagrangian formulation (solid material) and Eulerian formulation (gas medium) was performed. The latest extensive research in this area indicates that the finite element analyses of such problems require complex meshes for Euler and Lagrange formulation. This research is focused on Euler mesh density influence on coupled analysis results. The principal objective of this paper is to compare various mesh density Eulerian models in respect to accuracy and computing time and asses the limit of element size. The Eulerian domains (Air and HE) were developed with various element size from 10 mm up to 30 mm. Results from all the analysis cases show how the Eulerian mesh element size influences on the global response of the column. Models with coarse meshes give much lower dynamic response then models with finer meshes. The resultant velocity vectors were also presented to illustrate the characteristic of blast wave propagation. Moreover the numerical models computational efficiency was compared are respect of CPU Time. Models with complex meshes (below 20 mm) are very computationally expensive.
Źródło:
Journal of KONES; 2011, 18, 3; 245-252
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Numerical testing of landing gear system for different drop velocities
Autorzy:
Krasoń, W.
Małachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/245668.pdf
Data publikacji:
2009
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
landing gear
numerical simulation
drop velocities
touchdown
Opis:
The FEM model of the landing gear was developed to determine efforts of individual structural members while simulating the landing-gear drop, and to investigate how the energy of such a system changes; also, to find what kinds of deformations occur in individual components, and to investigate into the effectiveness of the damping system. In the developed numerical model of the landing gear account was taken also of the support-wheel-related subassembly, which includes such elements as: the wheel pin, the wheel rim, and the tyre. All parts of this subassembly, belt in the tyre excluded, were represented with the flexible hexagonal elements. results of numerical analyses for some selected drop tests and results from experiments carried out on a real landing gear confirm high quality of results gained from the dynamic simulation in the model of a complete landing-gear configuration. The advantage of the presented numerical method is applicability there of to landing gear testing for the very wide range of drop velocities, what is impossible to be performed with other methods, including experimental testing work. Paper show the geometric model of the main landing gear, a discrete model with the shock-absorber model included, the fringe of the landing gear deformation at the flnal stage of touchdown phase respectively from experimental and numerical tests and the maps ofmaximum principal stresses and how they change within the area of the welded joint that connects the upper and lower levers of the main landing gear.
Źródło:
Journal of KONES; 2009, 16, 4; 241-246
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Analysis of selected structural components subjected to blast wave
Autorzy:
Mazurkiewicz, Ł.
Małachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/248066.pdf
Data publikacji:
2012
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
ALE formulation
blast wave
dynamic response
structural component
Opis:
The phenomenon of high-energy explosion of a substance such as the mixture of flammable gases, explosives, etc. is highly exothermic chemical reaction that causes a blast wave consisting of hot gases at high pressure. Very complex nature of the phenomenon of detonation, affects the need for advanced methods of analysis. In the present work analysis of two steel columns (I-section and tubular section) subjected to the blast wave are presented. The columns have similar values of the moments of inertia and mass per unit length. To describe the complex phenomena occurring in gas medium the Eulerian formulation was used. The steel structures were described using Lagrangian formulation. Interaction between domains was achieved by numerical coupling algorithm with implemented penalty function. From the results from all the analysis cases, the dynamic response of structural elements was obtained. Permanent deformation and the amount of absorbed energy are of special interest in this study. The resultant velocity vectors were also presented to illustrate the characteristic of blast wave propagation.
Źródło:
Journal of KONES; 2012, 19, 1; 267-272
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Security improvement for oil and gas pipeline infrastructure
Autorzy:
Małachowski, J.
Gieleta, R.
Powiązania:
https://bibliotekanauki.pl/articles/244151.pdf
Data publikacji:
2008
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
security
simulation
modelling
Opis:
This research has been inspired by security concerns due to the recent increase in the terrorist threat to gas and crude oil transportation around the world, especially in regions that are of significant value for the energy supplies. Computational mechanics methods will be used in this research to apply shock wave analysis for possible damage assessment of the affected pipelines. These methods may be also used for pipelines at power plants (especially nuclear), which are usually placed high on the homeland security priority list. The main goal of this research is focused on establishing effective simulation methodology to study the influence of shock waves (caused by explosion) on pipeline systems (buried, on surface, or underwater) to ensure their security. This study is primarily focused on the behaviour of a pipeline subjected to the shock wave produced by the detonation of highly explosive (HE) materials. The results of this study will primarily allow for analysis of the blast wave propagation and the resulting damage inflicted by the pipeline. Outcomes of this research are important in preventing damage progression of pipelines under the blast loading. This data will also be used to develop improved design guidelines for safer and less vulnerable pipelines. The study allows for determining a type of structure of the high energy absorbing protective system.
Źródło:
Journal of KONES; 2008, 15, 2; 295-300
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Field test and numerical studies of the scissors-AVLB type bridge
Autorzy:
Krason, W.
Malachowski, J.
Powiązania:
https://bibliotekanauki.pl/articles/201143.pdf
Data publikacji:
2014
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
scissor-AVLB type bridge
experimental test
numerical FE analysis
Opis:
Scissor bridges are characterized by high mobility and modular structure. A single module-span consists of two spanning parts of the bridge; two main trucks and the support structure. Pin joints are used between modules of the single bridge span. Some aspects of the experimental test and numerical analysis of the scissor-AVLB type bridge operation are presented in this paper. Numerical analyses, presented here, were carried out for the scissors-type BLG bridge with treadways extended as compared to the classical bridge operated up to the present in the Armed Forces of the Republic of Poland. A structural modification of this kind considerably affects any changes in the effort of the force transmitting structure of the bridge. These changes may prove to be disadvantageous to the whole structure because of torsional moments that additionally load the treadways. Giving careful consideration to such operational instances has been highly appreciated because of the possibility of using this kind of bridges while organizing the crossing for vehicles featured with various wheel/track spaces (different from those used previously). The BLG bridge was numerically analysed to assess displacements and distributions of stresses throughout the bridge structure in different loading modes. Because of the complexity of the structure in question and simplifications assumed at the stage of constructing geometric and discrete models, the deformable 3D model of the scissors-type bridge needs verification. Verification of the reliability of models was performed by comparing deflections obtained in the different load modes that corresponded with tests performed on the test stand. It has been shown that the examined changes in conditions of loading the treadways of the bridge are of the greatest effect to the effort of the area of the joint which is attached to the girder bottom. Stress concentrations determined in the analysis are not hazardous to safe operation of the structure.
Źródło:
Bulletin of the Polish Academy of Sciences. Technical Sciences; 2014, 62, 1; 103-112
0239-7528
Pojawia się w:
Bulletin of the Polish Academy of Sciences. Technical Sciences
Dostawca treści:
Biblioteka Nauki
Artykuł
Wyświetlanie 1-15 z 59

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