Relevant bibliographies by topics / Vibration-damping materials and structures

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Vibration-damping materials and structures'

Author: Grafiati
Published: 4 June 2021
Last updated: 9 February 2022

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Journal articles on the topic "Vibration-damping materials and structures"

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Niwa, Takahiro, and Yasuo Shimizu. "Vibration damping materials and soundproofing structures using such damping materials." Journal of the Acoustical Society of America 92, no. 1 (July 1992): 626. http://dx.doi.org/10.1121/1.404088.

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Wagner, David A., Yuksel Gur, Susan M. Ward, and Marsha A. Samus. "Modeling Foam Damping Materials in Automotive Structures." Journal of Engineering Materials and Technology 119, no. 3 (July 1, 1997): 279–83. http://dx.doi.org/10.1115/1.2812257.

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Foam damping materials judiciously placed in automotive structures efficiently reduce the vibration amplitudes of large, relatively flat exterior body panels such as the hood, roof, deck lid (trunk) and door skin. These polymer foams (typically epoxy or vinyl) have mechanical properties that depend on the foam homogeneity, degree of expansion, temperature and frequency of excitation. Standard methods for determining true bulk mechanical properties, such as Young’s modulus, shear modulus and damping terms, are discussed along with methods for determining engineering estimates of the properties “as used” in automotive applications. Characterizing these foam damping materials in a component or full body finite element structural model as discrete springs and dashpots provides an accurate and economical means to include these features. Example analyses of the free vibrations and forced response of a hood are presented accompanied by test data that demonstrate the accuracy of the structural model. A parametric study investigates the effect of foam material stiffness and damping properties on hood vibration amplitudes under dynamic air loading. A methodology is discussed to reduce the hood vibration level under cross-wind conditions to an acceptable level with the use of foam materials.
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Kireitseu, Maksim. "Vibration Damping Properties of Nanotube-Reinforced Materials." Advances in Science and Technology 50 (October 2006): 31–36. http://dx.doi.org/10.4028/www.scientific.net/ast.50.31.

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Energy dissipation (damping) in structures/materials at the nanoscale level, the damping/ dynamics of materials require investigations before they will come to advanced engineering applications. By invoking the properties of nanostructures, it may be possible to enhance the energy dissipation. The paper therefore presents some preliminary results on the topic providing route map to the nanotechnology-based vibration damping solutions and comparison of some experimental damping behavior of nanoparticle-reinforced polymeric structures.
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Hujare, Pravin P., and Anil D. Sahasrabudhe. "Effect of Thickness of Damping Material on Vibration Control of Structural Vibration in Constrained Layer Damping Treatment." Applied Mechanics and Materials 592-594 (July 2014): 2031–35. http://dx.doi.org/10.4028/www.scientific.net/amm.592-594.2031.

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The reduction of noise and vibration is a major requirement for performance of any vibratory system. Passive damping technology using viscoelastic materials is classically used to control vibrations. Viscoelastic material among the damping materials is widely used to dissipate the structural vibration energy. Three-layer sandwich beams, made of two elastic outer layers and a viscoelastic layer sandwiched between them, are considered as damping structural elements. This paper presents the effect of thickness of constrained damping material on modal loss factor of vibrating structures. Measurements are performed on sandwich beam structure. In order to understand the effectiveness of the sandwich structures, the dynamics of beam with constrained viscoelastic layers are investigated. Comparisons of the experimental and the Numerical results confirm that the damping levels and the natural frequencies of damped structures are well corroborated.
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Kurosawa, Yoshio, and Takao Yamaguchi. "High Frequency Vibration Analysis of Automotive Body Panels with Damping Materials." Applied Mechanics and Materials 36 (October 2010): 293–96. http://dx.doi.org/10.4028/www.scientific.net/amm.36.293.

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We have developed a technique for estimating vibrations of an automotive body structures with viscoelastic damping materials using large-scale finite element (FE) model, which will enable us to grasp and to reduce high-frequency road noise（200～500Hz）. In the new technique, first order solutions for modal loss factors are derived applying asymptotic method. This method saves calculation time to estimate modal damping as a practical tool in the design stages of the body structures. Frequency responses were calculated using this technique and the results almost agreed with the test results. This technique can show the effect of the viscoelastic damping materials on the automotive body panels, and it enables the more efficient layout of the viscoelastic damping materials. Further, we clarified damping properties of the automotive body structures under coupled vibration between frames and panels with the viscoelastic damping materials.
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Tang, Li, Xiongliang Yao, Guoxun Wu, and Dong Tang. "Band Gaps Characteristics Analysis of Periodic Oscillator Coupled Damping Beam." Materials 13, no. 24 (December 16, 2020): 5748. http://dx.doi.org/10.3390/ma13245748.

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The vibration of the periodic oscillator coupled damping beam model is reduced through the band gaps designing method, which can be applied in equivalent engineering structures. In this paper, the flexural wave dispersion relations of the infinite long periodic oscillator coupled damping beam were calculated using the reverberation-ray matrix method combined with the Bloch theorem. The flexural wave vibration frequency response function of the finite long periodic oscillator coupled damping beam was carried out using the finite element method. The flexural wave vibration band gaps occur in the infinite long periodic oscillator coupled damping beam model in both the analytical and numerical results. In these band gaps, flexural waves’ propagation is prohibited, and flexural vibration is significantly suppressed. Furthermore, the effects of structure and material parameters on the flexural wave vibration band gaps characteristics are studied. Thus, the structural vibration reduction design can be realized by adjusting the related parameters of the periodic coupled damping beam structures and the equivalent 2D periodic stiffened plate structures.
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Lee, Jae Mun, Chul Hee Lee, and Seung Bok Choi. "Vibration Damping of Automotive Driveshafts with Piezofiber Composite Structures." Advanced Materials Research 47-50 (June 2008): 222–25. http://dx.doi.org/10.4028/www.scientific.net/amr.47-50.222.

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This paper presents a solution of the vibration reduction in driving automotive shafts. Generally, vibration modes in automotive driveshafts are divided into the bending and torsional vibrations. However, the bending vibration is more dominant factor when it excites with the resonance frequencies in automotive driveshafts. In this paper, the vibration damping structure of automotive driveshaft is introduced by incorporating piezofiber composite structure, which is also called as MFC (Macro Fiber Composite). The MFC is an innovative actuator that offers high performance and flexibility than other piezo-materials, so it is the best candidate of actuator to apply to the curved surface of shaft. In order to simulate the bending vibration reduction in the automotive shaft, analytical model based on cylindrical shell theory was developed. Moreover, Finite Element Analysis (FEA) using the piezoelectric-thermal analogy technique was conducted to confirm the analytical results and demonstrate the vibration reduction performance. The effect by the polarity of MFC on the vibration damping is also studied to find the best combination of MFC activation. Thus, the results showcase the optimal vibration damping capabilities using MFC in automotive driveshafts, and provide an outlook for the active damping control using the multi-mode resonance controllers.
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May, James E., and Craig Menzemer. "Modal damping effects on the spatial distribution of anelastic damped vibration energy for a baseline cantilever structure." Journal of Vibration and Control 18, no. 10 (October 26, 2011): 1575–82. http://dx.doi.org/10.1177/1077546311408990.

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Modal damping was conceived as a vibration control concept for potential application to a select set of long, flexible structures. This alternative approach was designed to exploit damping mechanisms inherent in the structures of interest by capitalizing on distinctive dynamic properties existing among vibration modes. The premise of modal damping is to transfer vibration energy from the fundamental mode where most vibration energy of civil structures of interest resides, to higher order modes where vibration impedance was shown to be more effective. A question was posed during its development concerning the subsequent risks to the structure. Spatial displacements, velocities and accelerations along the longitudinal axis will clearly be impacted and can readily be evaluated by simulation as required. The specific inquiry was directed at risks associated with redistribution of the damped vibration energy. In response, the distribution dynamics associated with the simple but ever-present anelastic damping mechanism was investigated and quantified. Furthermore, the analysis additionally offers support of the modal damping assertion by providing insight behind the increased dissipation effectiveness of the 2nd vibration mode over that of the fundamental mode.
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Yu, Jianda, Zhibo Duan, Xiangqi Zhang, and Jian Peng. "Wind-Induced Vibration Control of High-Rise Structures Using Compound Damping Cables." Shock and Vibration 2021 (April 22, 2021): 1–9. http://dx.doi.org/10.1155/2021/5537622.

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Based on the vibration reduction mechanism of compound damping cables, this study focuses on the wind-induced vibration control of high-rise structures with additional mass at the top. The differential equation of motion of the system under the action of the composite damping cable is established, and the analytical solution of the additional damping ratio of the structure is deduced, which is verified by model tests. The vibration response of the structure under the action of simple harmonic vortex excitation and randomly fluctuating wind loads is studied, and the effect of different viscous coefficients of the dampers in the composite damping cable and different installation heights of the damping cable on the vibration control is analyzed. The results show that a small vortex excitation force will cause large vibrations of low-dampened towering structures, and the structure will undergo buffeting under the action of wind load pulse force. The damping cable can greatly reduce the amplitude of structural vibration. The root means square of structural vibration displacement varies with damping. The viscosity coefficient of the device and the installation height of the main cable of the damping cable are greatly reduced.
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Zheng, Xiaoyuan, Zhiying Ren, Liangliang Shen, Bin Zhang, and Hongbai Bai. "Dynamic Performance of Laminated High-Damping and High-Stiffness Composite Structure Composed of Metal Rubber and Silicone Rubber." Materials 14, no. 1 (January 2, 2021): 187. http://dx.doi.org/10.3390/ma14010187.

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In this study, a laminated composite damping structure (LCDS) with metal rubber (MR) as matrix and silicone rubber (SR) as reinforcement has been designed. The embedded interlocking structure formed by the multi-material interface of the LCDS can effectively incorporate the high damping characteristics of traditional polymer damping materials and significantly enhance the adjustable stiffness of the damping structure. Based on the periodic cyclic vibration excitation, dynamic tests on different laminated structures were designed, and the damping performance and fatigue characteristics under periodic vibration excitation of the LCDS, based on MR and SR, were explored in depth. The experimental results exhibited that, compared to single-compound damping structures, the LCDS with SR as reinforcement and MR as matrix has excellent stiffness and damping characteristics. The incorporation of the silicon-based reinforcement can significantly improve the performance of the entire structure under cyclic fatigue vibration. In particular, the effects of material preparation and operating parameters on the composite structure are discussed. The effects of MR matrix density, operating frequency, amplitude, and preload on the stiffness and damping properties of the MR- and SR-based LCDS were investigated by the single factor controlled variable method. The results demonstrated that the vibration frequency has little effect on the LCDS damping performance. By increasing the density of the MR matrix or increasing the structural preload, the energy dissipation characteristics and damping properties of the LCDS can be effectively improved. With the increase in vibration excitation amplitude, the energy consumption of the LCDS increases, and the average dynamic stiffness changes at different rates, resulting in the loss factor decreasing first and then increasing. In this study, a damping structure suitable for narrow areas has been designed, which overcomes the temperature intolerance and low stiffness phenomena of traditional polymer rubber materials, and provides effective guidance for the design of damping materials with controllable high damping and stiffness.
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Dissertations / Theses on the topic "Vibration-damping materials and structures"

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Agnese, Fabio. "Enhanced vibration damping materials and structures for wind turbine blades inspired from auxetic configurations." Thesis, University of Bristol, 2014. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.653091.

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An extensive analysis of the current applications and possible employments of auxetic materials and configurations is presented. These novel materials show a negative Poisson's ratio and, potentially, enhanced mechanical properties. Despite a substantial amount of publications can be found in literature about auxetic material properties, not many of these consider practical applications for them. Objective and novelty of this project is therefore the application of auxetic material and/ or auxetic inspired configurations to existing structures and in particular to wind turbine blades to modify their dynamic characteristics. Wind turbine blades are complex systems manufactured using polymer matrix composite materials and at present made of a combination of glass and carbon fibre · reinforced plastic (GFRP-CFRP). Total damping in a blade is a combination of aerodynamic and structural loss factors, the latter being related to the inherent damping of the material. The two fundamental modes of vibration related to bending are of flapwise and edgewise type. The structural damping is material dependent, therefore the amount of structural damping available for these two vibration modes is the same. However, for the flapwise mode, the aerodynamic damping plays a very important role for the overall modal damping r.atio, whereas for the edgewise mode the only damping mechanism present is the str.uctural one. As a consequence, only a low value of loss factor can be achieved in the edgewise direction. The first aim of this project is then to demonstrate how auxetic inspired structure can be successfully applied to increase the loss factor of the blade in the edgewise direction of vibration. To this end several solutions have been investigated starting from the utilisation of 3D auxetic foams. They showed an effective increase in loss factor but limited by the fact that at present these foams present a low stiffness. Other solutions considered macro composites with shaped fibres and a novel damper design. Both these solutions have been analysed and characterised either by FE analysis and laboratory testing.
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Tremaine, Kellie Michelle. "MODAL ANALYSIS OF COMPOSITE STRUCTURES WITH DAMPING MATERIAL." DigitalCommons@CalPoly, 2012. https://digitalcommons.calpoly.edu/theses/823.

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The purpose of this study is to develop an analytical solution for modal analysis of actively damped orthotropic composite plates in bending and to verify it with experimental analysis. The analytical modal analysis solution for composite plate dynamics is derived using Euler theory. This analysis applies to structures with orthotropic lamina of uniform material properties at any lamination angle. The bending-extensional coupling can be neglected for plates that are symmetric or approximately symmetric, which allows an exact solution for natural frequency and mode shape to be obtained. An exact solution can be found for natural vibration and in general. The active control is modeled analytically by combining the Lagrange equation with the Ritz Assumed Mode method. This analysis produces a generalized coordinate vector that correlates the assumed mode to the particular amplitude of a particular case. The kinetic energy dissipated by the piezoelectric actuator from the system over one oscillation can be calculated from the generalized coordinate vector and the assumed mode. The equivalent damping ratio of the active control system is calculated as the ratio between the kinetic energy absorbed by the piezoelectric actuator from the system in one oscillation and the maximum strain energy of the system during that oscillation. A point mass on the plate, such as an accelerometer mass, can also be modeled as a single layer of uniform mass, that is an isotropic layer, by equating the potential energy of the point mass with the potential energy of the uniform mass layer. It is important to note that the mass of the isotropic layer is frequency dependent, and it has no effect on the plate stiffness. The analytical model is validated by comparison to experimental work. The samples studied were aluminum and composite plates of various lengths. The active control predictions were also validated using previous experimental work completed at California Polytechnic State University in San Luis Obispo. These cases included active control of an aluminum beam with a patch of piezoelectric material and an aluminum sailplane with a patch of piezoelectric material. Results indicate that while the analytical mode solutions are in good agreement with the experimental results, they are also systematically higher than the experimental results. The analytical active control solutions match previous work when the piezoelectric effects are linear. The main result of adding an active control system is approximately a 5-10% increase in modal frequencies and a 200-800% increase of damping ratio.
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Ao, Wai Kei. "Electromagnetic damping for control of vibration in civil structures." Thesis, University of Exeter, 2017. http://hdl.handle.net/10871/31145.

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This thesis investigates an alternative solution to deal with the civil structure vibration. Non-contact electromagnetic or Eddy current damping is selected as a score of vibration suppression. Electromagnetic damping relies on the interaction between a permanent magnet and conductor. An electromagnetic damper (EMD) is applied both to a laboratory footbridge structure and 6-storey model-scale aluminium moment resisting frame (AMRF). In this first study the EMD is connected in series with an electronic shunt circuit to construct an electromagnetic shunt damper (EMSD). A robust optimisation method is applied to develop the corresponding optimal design formula of the EMSD. The principle of an EMSD is to convert mechanical energy to electrical energy. Hence, the induced electromotive force (emf) is generated by electromagnetic induction. This emf induces an amount of shunt damping, which is fedback to the structure to achieve vibration suppression. It was found that when the impedance was applied, the shunt damping feature was of a similar nature to viscous dampers. In contrast, when an RLC (resistance-inductance-capacitance) circuit is connected, the shunt damping is analogous to a tuned mass damper. A second form of EMD is Eddy current damper (ECD), which relies on a geometrical arrangement of permanent magnets and conductors to produce damping forces. The vertical and horizontal orientation of the magnet, unidirectional and alternative pole projection and moving different direction of the conductor are investigated. A theoretical study involving the infinite boundary and finite boundary (the method of images current) is carried out to obtain an analytical calculation of the damping force. On the basis of this analysis, one type of ECD prototype was physically built. A performance test was carried out to determine the damping characteristics of the ECD, which agreed with the results of the numerical analysis. In addition, the ECD was applied to control the dynamics of the 6-storey AMRF. It was found that, the ECD can effectively increase system damping and have a satisfactory control effect.
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Li, Zhuang. "Vibration and acoustical properties of sandwich composite materials /." Auburn, Ala., 2005. http://repo.lib.auburn.edu/2005%20Fall/Dissertation/LI_ZHUANG_26.pdf.

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Verstappen, André Paul. "Passive damping treatments for controlling vibration in isotropic and orthotropic structural materials." Thesis, University of Canterbury. Mechanical Engineering, 2015. http://hdl.handle.net/10092/10197.

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The structural vibration damping behaviour of plates and beams can be improved by the application of viscoelastic passive damping materials. Unconstrained layer damping treatments applied to metal plate systems were studied experimentally. Design and modelling of novel fibre reinforced constrained layer damping materials was performed, and implementation of these composite damping materials into laminated composite sandwich constructions commonly used as structural elements within large composite marine vessels was explored. These studies established effective methods for examining, designing and applying damping materials to metal and composite marine structures. Two test fixtures were designed and constructed to facilitate testing of viscoelastic material damping properties to ISO 6721-3 and ASTM E756. Values of material damping made in accordance with ASTM E756 over a range of temperatures were compared to values produced by a Dynamic Mechanical Analyser (DMA). Glass transition temperatures and peak damping values were found to agree well, although results deviated significantly at temperatures above the glass transition temperature. The relative influence of damping layer thickness, ambient temperature, edge conditions, plate dimensions and substrate material on the system damping performance of metal plates treated with an unconstrained viscoelastic layer was investigated experimentally. This investigation found that substrate material had the greatest influence on system damping performance, followed by damping layer thickness and plate size. Plate edge conditions were found to have little influence on the measured system damping performance. These results were dependent on the values of each variable used in the study. Modal damping behaviour of a novel fibre reinforced composite constrained layer damping material was investigated using finite element analysis and experimental methods. The material consisted of two carbon fibre reinforced polymer (CFRP) layers surrounding a viscoelastic core. Opposing complex sinusoidal fibre patterns in the CFRP face sheets were used to achieve stress-coupling by way of orthotropic anisotopy about the core. A finite element model was developed in MATLAB to determine the modal damping, displacement, stress, and strain behaviour of these complex patterned fibre constrained layer damping (CPF-CLD) materials. This model was validated using experimental results produced by modal damping measurements on CPF-CLD beam test specimens. Studies of multiple fibre pattern arrangements found that fibre pattern properties and the resulting localised material property distributions influenced modal damping performance. Inclusion of CPF-CLD materials in laminated composite sandwich geometries commonly used in marine hull and bulkhead constructions was studied experimentally. Composite sandwich beam test specimens were fabricated using materials and techniques frequently used in industry. It was found that the greatest increases in modal damping performance were achieved when the CPF-CLD materials were applied to bulkhead geometries, and were inserted within the sandwich structure, rather than being attached to the surface.
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Lee, Yong Keat. "Active vibration control of a piezoelectric laminate plate using spatial control approach." Title page, abstract and table of contents only, 2005. http://hdl.handle.net/2440/37711.

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This thesis represents the work that has been done by the author during his Master of Engineering Science candidature in the area of vibration control of flexible structures at the School of Mechanical Engineering, The University of Adelaide, between March 2003 and June 2004. The aim of this research is to further extend the application of the Spatial Control Approach for two-dimensional flexible structures for attenuating global structural vibration with the possible implication of reduction in noise radiation. The research was concentrated on a simply supported thin flexible plate, using piezoelectric ceramic materials as actuators and sensors. In this work, active controllers were designed for the purpose of controlling only the first five vibration modes (0-500Hz) of the plate. A spatial controller was designed to minimize the total energy of the spatially distributed signal, which is reflected by the spatial H2 norm of the transfer function from the disturbance signal to the vibration output at every point over the plate. This approach ensures the vibration contributed by all the in bandwidth (0-500 Hz) vibration modes is minimized, and hence is capable of minimizing vibration throughout the entire plate. Within the control framework, two cases were considered here; the case when the prior knowledge of the incoming disturbance in terms of reference signal is vailable and the case when it is not available. For the case when the reference signal is available, spatial feedforward controller was designed; whereas for the case when the reference signal is not available, spatial feedback controller was designed to attenuate the global disturbance. The effectiveness of spatial controllers was then compared with that of the standard point-wise controllers numerically and experimentally. The experimental results were found to reflect the numerical results, and the results demonstrated that spatial controllers are able to reduce the energy transfer from the disturbance to the structural output across the plate in a more uniform way than the point-wise controllers. The research work has demonstrated that spatial controller managed to minimize the global plate vibrations and noise radiation that were due to the first five modes.
Thesis (M.Eng.Sc.)--School of Mechanical Engineering, 2005.
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Hegewald, Thomas. "Vibration Suppression Using Smart Materials in the Presence of Temperature Changes." Thesis, Virginia Tech, 2000. http://hdl.handle.net/10919/32068.

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Aircraft and satellite structures are exposed to a wide range of temperatures during normal operation cycles. These fluctuations in temperature may result in significant changes of the structural dynamics. Aircraft, automotive, and satellite structures are also subject to various vibration sources. Passive and active vibration suppression techniques have been developed to minimize acoustic noise and fatigue stress damage. Featuring low weight solutions and high performance, active control techniques are becoming increasingly common. Structures with varying dynamics require more sophisticated active control techniques, such as adaptive control.

This research uses a special vibration test rig for evaluating the performance of different vibration suppression systems on a representative aircraft panel. The test panel is clamped rigidly in a frame and can be excited in various frequencies with an electromagnetic shaker. To simulate temperature fluctuations the temperature on the panel can be increased up to 65°C (150°F). Smart material based sensors and actuators are used to interface the mechanical system with the electronic controller. The active controller utilizes three positive position feedback (PPF) filters implemented through a digital signal processor board. This research develops two different adaptation methods to perform vibration suppression in the presence of thermally induced frequency changes of the representative panel. To adjust the PPF filter parameters an open-loop adaptation method and an auto-tuning method are investigated. The open-loop adaptation method uses a measurement of the plate temperature and a look-up table with pre-determined parameters to update the filters accordingly. The auto-tuning methods identifies the frequencies of the poles and zeros in the structure's collocated transfer function. From the knowledge of the pole and zero locations the optimal PPF parameters are calculated online.

The results show that both adaptation methods are capable of reducing the vibration levels of the test specimen over the temperature range of interest. Three PPF filters with parameter adaptation through temperature measurement achieve magnitude reductions of the resonance peaks as high as 13.6 decibel. Using the auto-tuning method resonance peak reductions up to 17.4 decibel are possible. The pole/zero identification routine proves to detect the frequencies correctly. The average identification error remained at around one percent even in the presence of external disturbances.
Master of Science

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Hara, Deniz. "Investigation Of The Use Of Sandwich Materials In Automotive Body Structures." Master's thesis, METU, 2006. http://etd.lib.metu.edu.tr/upload/12614046/index.pdf.

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The use of sandwich structures in automobile body panels is investigated in this thesis. The applications on vehicles such as trains, aeroplanes and automobiles, advantages, isadvantages and modelling of sandwich structures are discussed and studies about static, vibrational and acoustic benefits of sandwich structures by several authors are presented. The floor, luggage, firewall and rear wheel panels in sheet metal form is replaced with panel made from sandwich materials in order to reduce the weight obtained by a trial and error based optimization method by keeping the same bending stiffness performance. In addition to these, the use of sandwich structures over free layer surface damping treatments glued on floor panel to decrease the vibration levels and air-borne noise inside the cabin is investigated. It has been proven that, the same vibration performance of both flat beam and floor panel can be obtained using sandwich structures instead of free layer surface damping treatments with a less weight addition. Furthermore, the damping effect of sandwich structures on sound transmission loss of complex shaped panels like floor panel is investigated. A 2D flat and curved panel representing the floor panel of FIAT Car model are analysed in a very large frequency range. Four different loss factors are applied on these panels and it is seen that, until it reaches damping controlled region, damping has a very little effect on TL of flat panels but has an obvious damping effect on TL of curved panels. However in that region, damping has an increasing effect on TL of both flat and curved panels.
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Ting, Joseph Ming-Shih. "Characterization of damping of materials and structures at nanostrain levels." Thesis, Massachusetts Institute of Technology, 1990. http://hdl.handle.net/1721.1/42439.

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Bravo, Rafael. "Vibration control of flexible structures using smart materials." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape4/PQDD_0034/NQ66256.pdf.

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Books on the topic "Vibration-damping materials and structures"

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Preumont, André. Vibration Control of Active Structures: An Introduction. Dordrecht: Springer Netherlands, 1997.

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Saravanos, D. A. Computational simulation of damping in composite structures. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

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Young, Maurice I. Structural dynamics and vibrations of damped, aircraft-type structures. Hampton, Va: Langley Research Center, 1992.

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Preumont, André. Vibration control of active structures: An introduction. Dordrecht: Kluwer Academic Publishers, 1997.

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Vibration control of active structures: An introduction. 2nd ed. Dordrecht: Kluwer Academic Publishers, 2002.

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Vibration control of active structures: An introduction. 3rd ed. Berlin: Springer, 2011.

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Preumont, André. Vibration control of active structures: An introduction. 2nd ed. Dordrecht: Kluwer Academic Publishers, 2002.

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Cortés, Fernando. Viscoelastic surface treatments for passive control of structural vibration. Hauppauge, N.Y: Nova Science Publishers, 2011.

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Saravanos, D. A. Multi-objective shape and material optimization of composite structures including damping. [Washington, D.C.]: NASA, 1990.

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Karnovsky, Igor A. Theory of Arched Structures: Strength, Stability, Vibration. Boston, MA: Springer Science+Business Media, LLC, 2012.

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Book chapters on the topic "Vibration-damping materials and structures"

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Kopp, Reiner, Marc Nutzmann, and Johan van Santen. "Formability of Lightweight, Vibration Damping and Medium Perfused Sandwich Sheets." In Sandwich Structures 7: Advancing with Sandwich Structures and Materials, 723–32. Dordrecht: Springer Netherlands, 2005. http://dx.doi.org/10.1007/1-4020-3848-8_73.

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Nakanishi, Yasumasa, Kin'ya Matsumoto, Masaru Zako, and Yukiko Yamada. "Finite Element Analysis of Vibration Damping for Woven Fabric Composites." In Advances in Composite Materials and Structures, 213–16. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-427-8.213.

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Rade, D. A., J. F. Deü, D. A. Castello, A. M. G. de Lima, and L. Rouleau. "Passive Vibration Control Using Viscoelastic Materials." In Nonlinear Structural Dynamics and Damping, 119–68. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-13317-7_5.

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Koona, Ramji, Ganesh Kumar, and S. Ranganath. "Optimization of Surface Damping Treatments for Vibration Control of Marine Structure." In Experimental Analysis of Nano and Engineering Materials and Structures, 747–48. Dordrecht: Springer Netherlands, 2007. http://dx.doi.org/10.1007/978-1-4020-6239-1_371.

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Lim, Teik-Cheng. "Vibration of Auxetic Solids." In Auxetic Materials and Structures, 345–65. Singapore: Springer Singapore, 2014. http://dx.doi.org/10.1007/978-981-287-275-3_11.

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Michael Sinapius, Johannes, Björn Timo Kletz, and Steffen Opitz. "Active Vibration Control." In Adaptronics – Smart Structures and Materials, 227–329. Berlin, Heidelberg: Springer Berlin Heidelberg, 2020. http://dx.doi.org/10.1007/978-3-662-61399-3_6.

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Chevalier, Yvon. "Damping in Materials and Structures: An Overview." In Advanced Structured Materials, 1–27. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-77504-3_1.

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Preumont, André. "Actuators, piezoelectric materials, and active structures." In Vibration Control of Active Structures, 32–59. Dordrecht: Springer Netherlands, 1997. http://dx.doi.org/10.1007/978-94-011-5654-7_3.

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Kaplunov, Julius, Danila A. Prikazchikov, and Olga Sergushova. "Lowest Vibration Modes of Strongly Inhomogeneous Elastic Structures." In Advanced Structured Materials, 265–77. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-56050-2_14.

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Shibuya, Yotsugi. "Evaluation of Internal Friction of Viscoelastic Composites with Meso-Scale Structures for Vibration Damping of Mechanical Structures." In Mechanics and Model-Based Control of Smart Materials and Structures, 163–72. Vienna: Springer Vienna, 2010. http://dx.doi.org/10.1007/978-3-211-99484-9_18.

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Conference papers on the topic "Vibration-damping materials and structures"

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HANAGUD, S., M. OBAL, and M. MEYYAPPA. "Electronic damping techniques and active vibration control." In 26th Structures, Structural Dynamics, and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-752.

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Sadri, A., R. Wynne, A. Cherry, A. Sadri, R. Wynne, and A. Cherry. "Robust active/passive damping for vibration suppression." In 38th Structures, Structural Dynamics, and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-1155.

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Feuchtwanger, Jorge, Kelli Griffin, Jian Kang Huang, Robert C. O'Handley, Samuel M. Allen, and David Bono. "Vibration damping in Ni-Mn-Ga composites." In Smart Structures and Materials, edited by Gregory S. Agnes and Kon-Well Wang. SPIE, 2003. http://dx.doi.org/10.1117/12.483795.

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Fu, Xuli, and Deborah D. L. Chung. "Vibration damping admixtures for cement." In 1996 Symposium on Smart Structures and Materials, edited by Conor D. Johnson. SPIE, 1996. http://dx.doi.org/10.1117/12.239085.

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Stuwing, Michael, Delf Sachau, and Elmar J. Breitbach. "Adaptive vibration damping of fin structures." In 1999 Symposium on Smart Structures and Materials, edited by Jack H. Jacobs. SPIE, 1999. http://dx.doi.org/10.1117/12.351571.

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Paulitsch, Christoph K., Paolo Gardonio, and Stephen J. Elliott. "Active vibration damping using a self-sensing electrodynamic actuator." In Smart Structures and Materials, edited by Kon-Well Wang. SPIE, 2004. http://dx.doi.org/10.1117/12.539737.

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Machado, Luciano G., and Dimitris C. Lagoudas. "Nonlinear dynamics of a SMA passive vibration damping device." In Smart Structures and Materials, edited by William W. Clark, Mehdi Ahmadian, and Arnold Lumsdaine. SPIE, 2006. http://dx.doi.org/10.1117/12.658062.

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Rogers, Lynn C., and Mike Parin. "Experimental results for stand-off passive vibration damping treatment." In Smart Structures & Materials '95, edited by Conor D. Johnson. SPIE, 1995. http://dx.doi.org/10.1117/12.208903.

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Baz, Amr M., and Jeng-Jong Ro. "Vibration control of plates with active constrained-layer damping." In Smart Structures & Materials '95, edited by Conor D. Johnson. SPIE, 1995. http://dx.doi.org/10.1117/12.208908.

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Wu, Shu-yau, and Andrew S. Bicos. "Structural vibration damping experiments using improved piezoelectric shunts." In Smart Structures and Materials '97, edited by L. Porter Davis. SPIE, 1997. http://dx.doi.org/10.1117/12.274217.

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Reports on the topic "Vibration-damping materials and structures"

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Yoshikawa, Shoko, R. Meyer, J. Witham, S. Y. Agadda, and G. Lesieutre. Passive Vibration Damping Materials: Piezoelectric Ceramic Composites for Vibration Damping Applications. Fort Belvoir, VA: Defense Technical Information Center, August 1995. http://dx.doi.org/10.21236/ada298477.

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Yoshikawa, Shoko, and S. K. Kurtz. Passive Vibration Damping Materials: Piezoelectric Ceramics Composites for Vibration Damping Applications. Fort Belvoir, VA: Defense Technical Information Center, February 1993. http://dx.doi.org/10.21236/ada260792.

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Wang, Kon-Well. Simultaneous Vibration Isolation and Damping Control Via High Authority Smart Structures. Fort Belvoir, VA: Defense Technical Information Center, January 2000. http://dx.doi.org/10.21236/ada424492.

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McDaniel, J. G., Kyle Bridgeo, and Hande Ozturk. Estimating the Effects of Damping Treatments on the Vibration of Complex Structures. Fort Belvoir, VA: Defense Technical Information Center, September 2012. http://dx.doi.org/10.21236/ada570547.

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Soovere, J., and M. L. Drake. Aerospace Structures Technology Damping Design Guide. Volume 3. Damping Material Data. Fort Belvoir, VA: Defense Technical Information Center, December 1985. http://dx.doi.org/10.21236/ada178315.

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Lagoudas, Dimitris C., Tamas Kalmar-Nagy, and Magdalini Z. Lagoudas. Shape Memory Alloys for Vibration Isolation and Damping of Large-Scale Space Structures. Fort Belvoir, VA: Defense Technical Information Center, August 2010. http://dx.doi.org/10.21236/ada564585.

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Inman, Daniel J. Vibration Analysis and Control of an Inflatable Structure Using Smart Materials. Fort Belvoir, VA: Defense Technical Information Center, August 2004. http://dx.doi.org/10.21236/ada425363.

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