Autor: Małachowski, J. - Katalog OPAC zbiorów

Skocz do pozycji: 1.

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

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Skocz do pozycji: 2.

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

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Skocz do pozycji: 3.

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

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Skocz do pozycji: 4.

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

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Skocz do pozycji: 5.

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

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Skocz do pozycji: 6.

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

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Skocz do pozycji: 7.

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

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Skocz do pozycji: 8.

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

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Skocz do pozycji: 9.

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

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Skocz do pozycji: 10.

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

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Skocz do pozycji: 11.

Tytuł:: Numerical investigation of a landing gear system with PIN joints operating clearance
Autorzy:: Krasoń, W.
Małachowski, J.
Sołtysiuk, J.
Powiązania:: https://bibliotekanauki.pl/articles/246952.pdf
Data publikacji:: 2010
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: landing gear
joints operating clearance
finite element method (FEM)
numerical simulation
Opis:: In this paper, FE method is applied to determine an operating clearance influence on the dynamics of a military transport aircraft landing gear. The numerical analysis results presentation of two-dimensional landing gear model drop tests using MSC Working Model code is also shown. Numerical results agree well with respective experimental investigation ones. The analyses using two-dimensional rigid model were performed to correlate a numerical characteristic of a shock absorber substitute model with real shock absorber characteristic. A fully deformable spatial discrete FEM model of the landing gear was developed for precise analyses aimed at determining a joint clearance influence on a considered mechanical system dynamics. Calculations were performed using the so-called direct-integration procedure, colloquially called 'the explicit integration'. Additionally at this stage, the Rayleigh damping model has been included. The non-linear dynamic analyses were performed using the LS-DYNA code. The final part presents the comparison of drop tests numerical solution results of a landing gear with assembly clearance and with operating clearance. The advantage of developed numerical method is the possibility to determine energy changing, particular components deformations, joint contact forces, what is nearly impossible to record performing experimental investigation. The presented method is applicable for a variety of boundary condition i.e. drop velocities, aircraft effective mass, etc.
Źródło:: Journal of KONES; 2010, 17, 2; 241-248
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 12.

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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Skocz do pozycji: 13.

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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Skocz do pozycji: 14.

Tytuł:: Numerical analysis of fluid flow in a syringe - test tube
Autorzy:: Krasoń, W.
Łazowski, J.
Małachowski, J.
Powiązania:: https://bibliotekanauki.pl/articles/246191.pdf
Data publikacji:: 2010
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: syringe
blood
flow
simulation
vorticity
Opis:: Numerical research in the field of collaboration of basic components and entire constructional solutions is much cheaper than managing a goods production and testing them in actual conditions. Numerical research allows determining essential modifications of a product being prepared from the functional, utilitarian and technological point of view. Considering the problem to be solved, the blood flows through the area limited by the sides of apiston, syringe and needle were analyzed. Pressure arises after the initiation of the piston's move and the blood flows as a result of the difference in pressures. The blood flows from the areas with higher pressure to the ones with lower pressure. The numerical research focused on analysis of the boundary conditions influence on the arrangement of the velocity and blood pressure in a syringe. In order to calculate the blond flow through a syringe the researchers used a model that allows the flow of adhesive fluids - substances with internal friction. Navier-Stokes' equations were used to describe adhesive fluids move mathematically. These equations allowed describing non-stationary flow of incompressible fluids, i.e. including no volumetric changes, however, including figural changes. In last analyzed case, i.e. with flow orifice, fluids dam up in front ofthe orifice and thenflow into the next chamberjust after the orifice. The fluids flow to the chamber as apiled up stream. Then, the fluids hit internal bend sides and rotate again in front of the needle orifice entry. Considering fluids parameters, vorticity process improves fluid mixing process.
Źródło:: Journal of KONES; 2010, 17, 1; 233-240
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 15.

Tytuł:: Influence of break shoes wearing in drum break - numerical approach
Autorzy:: Damaziak, K.
Jachimowicz, J.
Małachowski, J.
Powiązania:: https://bibliotekanauki.pl/articles/246894.pdf
Data publikacji:: 2010
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: road transport
simulation
brakes
thermal dynamic computations
Opis:: Braking system is one of the key components influencing passenger safety. Today, a design process of brakes is usually experience - driven, based on brake manufactures know - how. Using this approach, it is fairly difficult predict the brake components exact working condition or durability - parameters still more often required in a modern design process, what results in a rising demand for an exact simulation of a braking process. This paper presents numerical analyses of a drum brake. Both static and dynamic FE analyses were conducted in order to verify behaviour of numerical procedures affecting the braking process. The phenomena of heat generation by friction forces and the influence of a wear pattern was emphasized during dynamic calculations, while static analyses were focused on sensitivity to thermal properties of materials. FE models, including loads and boundary conditions, are described in details. Some of the data used during the simulation were taken from experiments. These laboratory tests are also briefly described in the paper. Based on the obtained results, it is shown that a numerical procedure converting sliding energy coming from friction to heat used in a coupled mechanical - thermal dynamic calculation works properly, but is very sensitive to material thermal properties. Proper FE modelling of the contact area and contact forces is also crucial. Unfortunately, due to lack of real material data, the presented results have quantitive character only.
Źródło:: Journal of KONES; 2010, 17, 2; 81-87
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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