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Abstract

The aim of this paper is to present an assessment of the slip influence on the deflection of the steel plate-concrete composite beams, which are a new type of a design concept. The proposed method is based on the procedure included in the PN-EN 1992-1-1, which has been modified with taking into consideration interface slip. The theoretical analysis was verified by experimental studies.

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Authors and Affiliations

D. Kisała
K. Furtak
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Abstract

Introduction of polymers into the cement composites improves same of the properties of concretes and mortars. Therefore, the polymer-cement composites are successfully used in construction. The model of microstructure formation in cement composites modified with thermoplastic polymer (pre-mix modifiers) has already been developed and successfully implemented. However, the formation of microstructure in the case of epoxy-cement composites (containing post-mix modifier) demonstrates same peculiarities which should be taken into account when modelling the process. The microstructure of epoxy-cement composites and its formation is discussed in the paper. The model is offered, formulated on the basis of the microscopic observations and results of testing.

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Authors and Affiliations

P. Łukowski
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Abstract

In this stud y, we attempt to analyse free nonlinear vibrations of buckling in laminated composite beams. Two new methods are applied to obtain the analytical solution of the nonlinear governing equation of the problem. The effects of different parameters on the ratio of nonlinear to linear natural frequencies of the beams are studied. These methods give us an agreement with numerical results for the whole range of the oscillation amplitude.

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Authors and Affiliations

G. Abdollahzadeh
M. Ahmadi
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Abstract

The paper presents the response of a three-layered annular plate with damaged laminated facings to the loads acting in their planes. The presented problem concerns the analysis of the combination of global plate failure in the form of buckling with the local micro defects, like fibre or matrix cracks, located in the laminas. The plate structure consists of thin laminated, fibre-reinforced composite facings and a thicker foam core. The matrix and fibre cracks of facings laminas can be transversally symmetrically or asymmetrically located in plate structure. Critical static and dynamic stability analyses were carried out solving the problem numerically and analytically. The numerical results show the static and dynamic stability state of the composite plate with different combinations of damages. The final results are compared with those for undamaged structure of the plate and treated as quasi-isotropic ones. The analysed problem makes it possible to evaluate the use of the non-ideal composite plate structure in practical applications.

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Bibliography

[1] Y.R. Chen, L.W. Chen and C.C. Wang. Axisymmetric dynamic instability of rotating polar orthotropic sandwich annular plates with a constrained damping layer. Composite Structures, 73(1):290–302, 2006. doi: 10.1016/j.compstruct.2005.01.039.
[2] H.J. Wang, L.W. Chen. Axisymmetric dynamic stability of rotating sandwich circular plates. Journal of Vibration and Acoustics, 126(2):407–415, 2004. doi: 10.1115/1.1688765.
[3] A. Wirowski. Tolerance modelling of dynamics of microheterogeneous annular plates. Monograph of the Technical University of Łódz, Łódz, 2016 (in Polish).
[4] J. Je. Axisymmetric buckling analysis of homogeneous and laminated annular plates. International Journal of Pressure Vessels and Piping, 62(1):153–159, 1995. doi: 10.1016/0308-0161(94)00004-3.
[5] J. Ye. Laminated Composite Plates and Shells. Springer-Verlag, London, 2003.
[6] H.J. Ding and R.Q. Xu. Exact solution for axisymmetric deformation of laminated transversely isotropic annular plates. Acta Mechanica, 153(1-2):169-182, 2002. doi: 10.1007/BF01177450.
[7] R. Lal and R. Rani. Axisymmetric vibrations of composite annular sandwich plates of quadratically varying thickness by harmonic differential quadrature method. Acta Mechanica, 226(5):1993-2012, 2015. doi: 10.1007/s00707-014-1284-0.
[8] J. Lee and C. Soutis. Prediction of impact-induced fibre damage in circular composite plates. Applied Composite Materials, 12(1):109–131, 2005. doi: 10.1007/s10443-004-7767-8.
[9] A. Muc and P. Zuchara. Buckling and failure analysis of FRP faced sandwich plates. Composite Structures, 48(1-3):145–150, 2000. doi: 10.1016/S0263-8223(99)00087-2.
[10] L.P. Khoroshun and D.V. Babich. Stability of plates made of fibrous composite with components subject to long-term damage. I nternational Applied Mechanics, 46(4):573–579, 2010. doi: 10.1007/s10778-010-0343-z.
[11] P. Maimi, P.P. Camanho, J.A. Mayugo, and A. Turon. Matrix cracking and delamination in laminated composites. Part II: Evaluation of crack density and delamination. Mechanics of Materials, 43(3):194–211, 2011. doi: 10.1016/j.mechmat.2011.01.002.
[12] A. Ahmed and L.J. Sluys: Computational modelling of impact damage in laminated composite plates. ECCM-16-th European Conference on Composite Materials, Seville, Spain, 22–26 June, 2014.
[13] F. Tornabene, N. Fantuzzi, M. Bacciocchi, and E.Viola. Mechanical behaviour of damaged laminated composites plates and shells: Higher-order Shear Deformation Theories. Composite Structures, 189:304–329, 2018. doi: 10.1016/j.compstruct.2018.01.073.
[14] F. Tornabene, N. Fantuzzi, and M. Bacciocchi. Linear static behaviour of damaged laminated composite plates and shells. Materials, 10(7):811, 2017. doi: 10.3390/ma10070811.
[15] Q. Meng and Z. Wang. Micromechanical modeling of impact damage mechanisms un unidirectional composite laminates. Applied Composite Materials, 23(5):1099-1116, 2016. doi: 10.1007/s10443-016-9502-7.
[16] A. De Luca, F. Caputo, Z. Sharif Khodaei, and M.H. Aliabadi. Damage characterization of composite plates under low velocity impact using ultrasonic guided waves. Composites Part B: Engineering, 138:168–180, 2018. doi: 10.1016/j.compositesb.2017.11.042.
[17] S.T. Rokotonarivo, C. Payan, J. Moysan, and C. Hochard. Local damage evaluation of a laminate composite plate using ultrasonic birefringence of shear wave. Composites Part B: Engineering, 142:287–292, 2018. doi: 10.1016/j.compositesb.2018.01.006.
[18] A. Ghosh and P.K. Sinha. Dynamic and impact response of damaged laminated composite plates. Aircraft Engineering and Aerospace Technology, 7(1):29–37, 2004. doi: 10.1108/00022660410514982.
[19] K.S. Sivakumaran. Free vibration of annular and circular asymmetric composite laminates. Composite Structures, 11(2):205–226, 1989. doi: 10.1016/0263-8223(89)90059-7.
[20] D. Pawlus. Stability of three-layered annular plate with composite facings. Applied Composite Materials, 24(1):141–158, 2017. doi: 10.1007/s10443-016-9518-z.
[21] D. Pawlus. Evaluation of critical static loads of three-layered annular plates with damaged composite facings. Engineering Transactions, 64(3):613–619, 2016.
[22] D. Pawlus. Dynamic response of three-layer annular plate with damaged composite facings. Archive of Mechanical Engineerig, 65(1):1: 83–105, 2018. doi: 10.24425/119411.
[23] D. Pawlus. Critical state evaluation of three-layered annular plates with symmetry and asymmetry damaged composite structure. Mechcomp 3 – 3rd International Conference on Mechanics of Composites, Bologna, Italy, 4–7 July, 2017.
[24] A. Muc. Mechanics of Fibrous Composites. Księgarnia Akademicka, Kraków, 2003 (in Polish).
[25] C. Volmir. Nonlinear Dynamic of Plates and Shells. Science, Moskwa, 1972 (in Russian).
[26] J. German. Fundamentals of Mechanics of Fibrous Composites. Politechnika Krakowska, Kraków, 1996 (in Polish).
[27] R.M. Jones. Mechanics of Composite Materials. Scripta Book Company, Washington D.C., 1975.
[28] D. Pawlus. Dynamic Stability of Three-Layered Annular Plates with Viscoelastic Core. Scientific Bulletin of the Technical University of Łódz, 1075, Łódz, 2010. (in Polish).
[29] D. Pawlus. Dynamic stability of three-layered annular plates with wavy forms of buckling. Acta Mechanica, 216(1-4):123–138, 2011. doi: 10.1007/s00707-010-0352-3.
[30] D. Pawlus. Solution to the problem of axisymmetric and asymmetric dynamic instability of three-layered annular plates. Thin-Walled Structures, 49(4):660–668, 2011. doi: 10.1016/j.tws.2010.09.013.
[31] Dynamic Stability of Composite Plate Construction, K. Kowal-Michalska, editor. WNT, Warszawa, 2007 (in Polish).
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Authors and Affiliations

Dorota Pawlus
1

  1. Faculty of Mechanical Engineering and Computer Science, University of Bielsko-Biala, Poland.
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Abstract

This paper presents an experimental analysis of flexural capacity and deformability of structural concrete slabs prepared as composite members consisting of two concrete layers made of reinforced ordinary concrete (N) and fiber reinforced concrete (SFRC). The reinforced concrete composite slabs used in the tests were prepared in the dimensions of 600 x 1200 x 80 mm. The basis was composed of two layers consisting of SFRC, one as the top layer, and one as ordinary concrete. The results of the analysis confirm a significant improvement of structural properties of the composite slab in comparison to the slabs prepared wholly of ordinary concrete.

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Authors and Affiliations

B. Sadowska-Buraczewska
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Abstract

This paper presents research results of composite tubes filled with self-compacting concrete. The impact of the selected materials and geometric factors on resistance to the vertical shear was evaluated in this study. The resistance of the tested members was compared with recommendations given in Eurocode PN-EN 1994-1-1. From the results obtained in the tests it can be deduced that more parameters should be taken into consideration when determining resistance to the vertical shear in the interface between steel and concrete than PN-EN 1994-1-1 recommends.

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Authors and Affiliations

M. Szadkowska
E. Szmigiera
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Abstract

This paper presents matters related to production of ceramic and cast iron composite. The composite was made with the use of a foam structured ceramic insert. The tests included measuring of hardness, impact strength and resistance to abrasive wear of the composite produced. On the basis of obtaining results was stated that the use of foamed ceramic filters provides good conditions of filling a ceramic framework with molten grey or chromium cast iron. The growth of hardness of the ceramic- grey cast iron composite is ca. 60% as compared to the grey cast iron hardness. The growth of hardness of the ceramic- chromium cast iron composite is slight and does not exceed 5 % in comparison to the chromium cast iron. Introduction of the ceramic inserts deteriorates the cast iron impact strength by ca. 20 - 30 %. The use of ceramic inserts increases the resistance to abrasive wear in case of grey cast iron by ca. 13% and in case of the chromium cast iron by ca. 10 %.
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Authors and Affiliations

A. Dulska
A. Studnicki
M. Cholewa
J. Szajnar
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Abstract

Definition of a composite [1] describes an ideal composite material with perfect structure. In real composite materials, structure is usually imperfect – composites contain various types of defects [2, 3–5], especially as the casted composites are of concern. The reason for this is a specific structure of castings, related to course of the manufacturing process. In case of metal matrix composite castings, especially regarding these manufactured by saturation, there is no classification of these defects [2, 4]. Classification of defects in castings of classic materials (cast iron, cast steel, non-ferrous alloys) is insufficient and requires completion of specific defects of mentioned materials. This problem (noted during manufacturing metal matrix composite castings with saturated reinforcement in Institute of Basic Technical Sciences of Maritime University Szczecin) has become a reason of starting work aimed at creating such classification. As a result, this paper was prepared. It can contribute to improvement of quality of studied materials and, as a consequence, improve the environment protection level.

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Authors and Affiliations

K. Gawdzińska
D. Nagolska
M. Szweycer
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Abstract

The multiple direct remelting of composites based on the A359 alloy reinforced with 20% of Al2O3 particles was performed. The results of both gravity casting and squeeze casting were examined in terms of the obtained microstructure and mechanical characteristics. In microstructure examinations, the combinatorial method based on phase quanta theory was used. In mechanical tests, the modified low cycle fatigue method (MLCF) was applied. The effects obtained after both gravity casting and squeeze casting were compared. It was noted that both characteristics were gradually deteriorating up to the tenth remelting. The main cause was the occurrence of shrinkage porosity after the gravity casting. Much better results were obtained applying the squeeze casting process. The results of microstructure examinations and fatigue tests enabled drawing the conclusion that the A359 alloy reinforced with Al2O3 particles can confer a much better fatigue life behavior to the resulting composite than the A359 alloy without the reinforcement. At the same time, comparing these results with the results of the previous own research carried out on the composites based also on the A359 alloy but reinforced in the whole volume with SiC particles, it has been concluded that both types of the composites can be subjected to multiple remelting without any significant deterioration of the structural and mechanical characteristics. The concepts and advantages of using the combinatorial and MLCF methods in materials research were also presented
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Authors and Affiliations

M. Maj
K. Pietrzak
A. Klasik
J. Sobczak
A. Wojciechowski
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Abstract

The quest for airframe weight reduction results in a careful dimensioning cross section areas of structural airframe components depending on the anticipated loading. In the case of flanges of polymeric laminate spars subjected to tension such a dimensioning can be done by means of appropriate ply dropping along the spar flanges. A method for an effective calculation of the number of plies that can be cut off at the cross-section under consideration without excessive stress concentration resulted has been presented. The method takes advantage of the Linear Fracture Mechanics tools combined with simple finite element calculations. In addition, experimental data needed can be easily obtained with the use of inexpensive specimens that are simple for manufacturing and testing.

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Authors and Affiliations

Piotr Czarnocki
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Abstract

This paper presents the capabilities of ABAQUS finite-element program [1] in modelling sandwich beams and plates resting on deformable foundations. Specific systems of sandwich beams and plates separated by an elastic core layer were subjected to the action of point and distributed moving loads. A few theoretical examples are provided to present different techniques of modelling the foundations and the moving loads. The effects of the boundary conditions and of the foundation parameters on the deflections of the analysed structures are also presented.

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Authors and Affiliations

A. Zbiciak
M. Ataman
W. Szcześniak
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Abstract

This paper investigates the behaviour of axially-loaded tubular columns filled with M20 grade concrete and partially replaced concrete. The parameters varying in the study are slenderness ratio (13.27, 16.58 & 19.9), and normal M20 grade concrete, partially replaced quarry dust and concrete debris. The effects of the various concrete mixes and composite action between the steel tube and the concrete core are studied and a graph visualizing the differences between the load carrying capacity and the axial deflection is plotted. Some of the performance indices like the Ductility Index (DI), Concrete Contribution Ratio (CCR), Confinement Index (θ) and Strength Index (SI) are also evaluated and compared amongst the CFST columns. From the results it has been noted that an increase in the L/D ratio decrease the behaviour of the composite columns irrespective of the in filled materials. The composite action was achieved in the CFST columns filled with partially replaced quarry dust and concrete debris when compared with hollow steel columns. The load carrying capacity of the CFST column increases by 32 % compared with the hollow tubular columns.

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Authors and Affiliations

P. Sangeetha
R. Senthil
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Abstract

Buckling and postbuckling response of thin-walled composite plates investigated experimentally and determinated analytically and numerically is compared. Real dimension specimens of composite plates weakened by cut-out subjected to uniform compression in laboratory buckling tests have been modelled in the finite element method and examined analytically based on P-w2 and P-w3 methods. All results were obtained during the experimental investigations and the numerical FEM analysis of a thin-walled composite plate made of a carbon-epoxy laminate with a symmetrical eight-layer arrangement of [90/-45/45/0]s. The instrument used for this purpose was a numerical ABAQUS® program.

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Authors and Affiliations

K. Falkowicz
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Abstract

The paper presents selected granular ceramic materials available on the Polish market. Their characteristics have been determined in the aspect on application in the production of iron alloy-ceramic composite. The possibility of obtaining a composite layer by means of bulk grains in molds of plates were considered, which was the foundation for experimental molds to be used in service tests. On the basis of obtaining results was stated that the knowledge of the characteristics of bulk grains enables the calculation of their quantity necessary for the composite production. When using the bulk grains the thickness of the composite layer is restricted by the thermal relations (cooler) and the physical phenomena (buoyancy, metal static pressure). Increasing amount of grains above definite condition causes surface defects in the castings. Each casting, due to its weight, shape and place of composite layer production requires an individual approach, both at the stage of formation and that of calculation of the required quantity of ceramic grains.
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Authors and Affiliations

A. Dulska
J. Kilarski
A. Studnicki
J. Szajnar
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Abstract

The paper presents results of compressive strength investigations of EN AC-44200 based aluminum alloy composite materials reinforced

with aluminum oxide particles at ambient and at temperatures of 100, 200 and 250C. They were manufactured by squeeze casting of the

porous preforms made of α-Al2O3 particles with liquid aluminum alloy EN AC-44200. The composite materials were reinforced with

preforms characterized by the porosities of 90, 80, 70 and 60 vol. %, thus the alumina content in the composite materials was 10, 20, 30

and 40 vol.%. The results of the compressive strength of manufactured materials were presented and basing on the microscopic

observations the effect of the volume content of strengthening alumina particles on the cracking mechanisms during compression at

indicated temperatures were shown and discussed. The highest compressive strength of 470 MPa at ambient temperature showed

composite materials strengthened with 40 vol.% of α-Al2O3 particles.

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Authors and Affiliations

A. Kurzawa
J.W. Kaczmar
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Abstract

Diagnostics of composite castings, due to their complex structure, requires that their characteristics are tested by an appropriate description

method. Any deviation from the specific characteristic will be regarded as a material defect. The detection of defects in composite castings

sometimes is not sufficient and the defects have to be identified. This study classifies defects found in the structures of saturated metallic

composite castings and indicates those stages of the process where such defects are likely to be formed. Not only does the author

determine the causes of structural defects, describe methods of their detection and identification, but also proposes a schematic procedure

to be followed during detection and identification of structural defects of castings made from saturated reinforcement metallic composites.

Alloys examination was conducted after technological process, while using destructive (macroscopic tests, light and scanning electron

microscopy) and non-destructive (ultrasonic and X-ray defectoscopy, tomography, gravimetric method) methods. Research presented in

this article are part of author’s work on castings quality.

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Authors and Affiliations

K. Gawdzińska
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Abstract

The Copper-SiC composite was investigated with the help of FEM. The authors modeled and analyzed the effect of relaxation of thermal stresses due to seasoning at room temperature after the manufacturing process together with the effect of thermal stresses induced by reheating the material to a service temperature. Especially, hypothetical fracture at interface was of interest. It was shown that, for a fixed temperature, a single crack emanating at 0° or 45° azimuth would develop only along a portion of fiber perimeter, and a further growth would require stress increase in the fiber surrounding.

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Authors and Affiliations

Piotr Czarnocki
Grzegorz Krzesiński
Piotr Marek
Tomasz Zagrajek
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Abstract

The paper describes the dynamics of a composite cantilever beam with an active element. The vibrations of the kinematically excited beam are controlled with the use of a Macro Fiber Composite actuator. A proportional control algorithm is considered. During the analysis, actuator is powered by a time-varying voltage signal that is changed proportionally to the beam deflection. The MFC element control system with the implemented algorithm allowed for changing the stiffness of the tested structure. This is confirmed by the numerical and experimental results. Resonance curves for the beam with and without control are determined. The results show a very good agreement in qualitative terms.

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Bibliography

[1] R.B.Williams, G. Park, D.J. Inman, and W.K.Wilkie. An overview of composite actuators with piezoceramic fibers. In: Proceedings of 20th International Modal Analysis Conference, Los Angeles, CA, 4–7 February, 2002, SPIE – The International Society for Optical Engineering, 4753:421–427, 2002.
[2] B.W. Lacroix. On the mechanics, computational modeling and design implementation of piezoelectric actuators on micro air vehicles. Ph.D. Thesis, University of Florida, Gainesville, USA, 2013.
[3] T.A. Probst. Evaluating the Aerodynamic Performance of MFC-Actuated Morphing Wings to Control a Small UAV. Masters Thesis, Virginia Polytechnic Institute and State University, Blacksburg, USA, 2012.
[4] M. Borowiec, M. Bochenski, J. Gawryluk, and M. Augustyniak. Analysis of the macro fiber composite characteristics for energy harvesting efficiency. In: Awrejcewicz J., editor, Dynamical Systems: Theoretical and Experimental Analysis, vol. 182 of Springer Proceedings in Mathematics and Statistics Series, pages 27–37, 2016. doi: 10.1007/978-3-319-42408-8_3.
[5] J. Latalski. Modelling of macro fiber composite piezoelectric active elements in ABAQUS system. Eksploatacja i Niezawodność – Maintenance and Reliability, 52(4):72–78, 2011.
[6] A. Teter and J. Gawryluk. Experimental modal analysis of a rotor with active composite blades. Composite Structures, 153:451–467, 2016. doi: 10.1016/j.compstruct.2016.06.013.
[7] J. Gawryluk, A. Mitura, and A. Teter. Influence of the piezoelectric parameters on the dynamics of an active rotor. AIP Conference Proceedings, 1922(100010):1–8, 2018. doi: 10.1063/1.5019095.
[8] A. Mitura, J. Gawryluk, and A. Teter. Numerical and experimental studies on the rotating rotor with three active composite blades. Eksploatacja i Niezawodność – Maintenance and Reliability, 4(19):572–581, 2017. doi: 10.17531/ein.2017.4.11.
[9] J. Gawryluk, A. Mitura, and A. Teter. Dynamic response of a composite beam rotating at constant speed caused by harmonic excitation with MFC actuator. Composite Structures, 210:657–662, 2019. doi: 10.1016/j.compstruct.2018.11.083.
[10] M. Rafiee, F. Nitzsche, and M. Labrosse. Dynamics, vibration and control of rotating composite beams and blades: A critical review. Thin-Walled Structures, 119:795–819, 2017. doi: 10.1016/j.tws.2017.06.018.
[11] R. Alkhatib and M.F. Golnaraghi. Active structural vibration control: a review. The Shock and Vibration Digest, 35(5):367–383, 2003.
[12] P.P. Friedmann. On-blade control of rotor vibration, noise, and performance: just around the corner? Journal of the American Helicopter Society, 59(4):1–37, 2014. doi: 10.4050/JAHS.59.041001.
[13] J.X. Gao and W.H. Liao. Vibration analysis of simply supported beams with enhanced selfsensing active constrained layer damping treatments. Journal of Sound and Vibration, 280(1-2):329–357, 2005. doi: 10.1016/j.jsv.2003.12.019.
[14] J.C. Lin and M.H. Nien. Adaptive control of a composite cantilever beam with piezoelectric damping-modal actuators/sensors. Composite Structures, 70(2):170–176, 2005. doi: 10.1016/j.compstruct.2004.08.020.
[15] H.A. Sodano. Macro-Fiber Composites for Sensing, Actuation and Power Generation. Masters Thesis, Virginia Polytechnic Institute and State University, Blacksburg, USA, 2003.
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Authors and Affiliations

Jarosław Gawryluk
1
Andrzej Mitura
1
Andrzej Teter
1

  1. Department of Applied Mechanics, Mechanical Engineering Faculty, Lublin University of Technology, Lublin, Poland.
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Abstract

In this study, the vibration analysis of fully and partially treated laminated composite Magnetorheological (MR) fluid sandwich plates has been investigated experimentally. The natural frequencies of fully and partially treated laminated composite MR fluid sandwich plates have been measured at various magnetic field intensities under two different boundary conditions. The variations of natural frequencies with applied magnetic field, boundary conditions and location ofMRfluid pocket have been explored. Further, a comparison of natural frequencies of fully and partially treated MR fluid sandwich structure has been made at various magnetic field intensities.

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Authors and Affiliations

R. Manoharan
R. Vasudevan
P. Edwin Sudhagar
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Abstract

Polymer composite materials based on the Moplen HP400R polypropylene matrix with a filler from walnut shell flour with 30, 40 and 50% content and 200-315 µm and 315-443 µm fraction were produced by the injection method. The effect of filler content was analysed on the processing properties of the composites such as: MFR Melt Flow Rate and the MVR Melt Volume-flow Rate, as well as the temperature of the filler flour decomposition using the TGA thermogravimetric analysis method. The following was also determined: density, hardness, tensile strength and stiffness modulus of elasticity of the materials in question. The obtained composite material was characterised by low density, which increased with the rising filler content. It was found that the applied natural filler has increased the hardness and stiffness modulus of the composite and decreased the tensile strength.

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Authors and Affiliations

A. Włodarczyk-Fligier
M. Polok-Rubiniec
B. Chmielnicki
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Abstract

This study focuses to develop a new hybrid Engineered Cementitious Composite (ECC) and assesses the performance of a new hybrid ECC based on the steel short random fiber reinforcement. This hybrid ECC aims to improve the tensile strength of cementitious material and enhance better flexural performance in an RC beam. In this study, four different mixes have been investigated. ECC with Poly Vinyl Alcohol (PVA) fiber and PolyPropylene (PP) fiber of 2.0% volume fraction are the two Mono fiber mixes; ECC mix with PVA fiber of 0.65% volume fraction hybridized with steel fiber of 1.35% volume fraction, PP fiber of 0.65% volume fraction hybridized with steel of 1.35% volume fraction are the two additional different hybrid mixes. The material properties of mono fiber ECC with 2.0 % of PVA is kept as the reference mix in this study. The hybridization with fibers has a notable achievement on the uniaxial tensile strength, compressive strength, Young’s modulus, and flexural behavior in ECC layered RC beams. From the results, it has been observed that the mix with PVA fiber of 0.65% volume fraction hybrid with steel fiber of 1.35% volume fraction exhibitimprovements in tensile strength, flexural strength, andenergy absorption. ThePP fiber of 0.65% volume fraction hybridized with steel of 1.35% volume fraction mix has reasonable flexural performance and notable achievement in displacement ductility overthe reference mix.

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Authors and Affiliations

A.R. Krishnaraja
Dr.S. Kandasamy
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Abstract

Transient heat transfer is studied and compared in two plane-parallel composite walls and one EPIDIAN 53 epoxy resin wall acting as a matrix for both composites. The first of the two walls is made of carbon-epoxy composite; the other wall is made of glass-epoxy composite, both with comparable thickness of about 1 mm and the same number of carbon and glass fabric layers (four layers). The study was conducted for temperatures in the range of 20-120 °C. The results of the study of thermal diffusivity which characterizes the material as a heat conductor under transient conditions have a preliminary character. Three series of tests were conducted for each wall. Each series took about 24 h. The results from the three series were approximated using linear functions and were found between (0.7-1.35) x 10-7m2/s. In the whole range of temperature variation, the thermal diffusivity values for carbon-epoxy composite are from 1.2 to 1.5 times higher than those for the other two materials with nearly the same thermal diffusivity characteristics.
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Authors and Affiliations

Janusz Terpiłowski
Joanna Piotrowska-Woroniak
Julita Romanowska
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Abstract

A method of calculating the deflections of steel plate-concrete composite beams is proposed. In the hybrid work of such beams the properties of reinforced concrete and composite structures are combined. This convention should be followed in considering their ultimate capacity and serviceability limit state. The proposed solution has been verified in experimental studies performed by the authors. Good compatibility of theoretical calculations and experimental results has been obtained. It allows the theoretical solution to be used in the analysis of other cases with parameters different than those of the discussed beams. In the experiments done by the author six beams of total length of 5.20 m and theoretical length of 5,00 m were used. The cross section was rectangular, 0.24 m in width and 0.49 m in height. The steel plate 4.74 m long was 6.10 and 16 mm thick. The diameter of the flexible connectors was 13 mm. Their spacing varied between 80 and 200 mm. Owing to the flexibility of the connectors the interface slip between the steel and concrete parts was included in the theoretical solutions. The results of an in-depth analysis indicate that the deflections of steel plate-concrete composite beams are affected by the compressive strength of concrete and the yield point of steel as well as connectors’ diameter and spacing. This impact varies, that of the yield point of the steel from which the plate is made being the highest.
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Authors and Affiliations

Dawid Kisała
1
Kazimierz Furtak
1
ORCID: ORCID

  1. Department of Bridge and Tunnel Building, Tadeusz Kościuszko Cracow University of Technology, Warszawska 24 St., 31-155 Kraków, Poland

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