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Applications of composites

COMBINED APPLICATION OF COMPOSITION AND STRUCTURE ANALYSIS METHODS TO THE DETERMINATION OF MAGNESIUM CONCENTRATION AND LOCATION IN BONE... [Pg.39]

Since weight is frequently a factor in the applications of composite structures, values for eleetrical and thermal conductivity, and tensile strength and modulus are even more impressive when normalized by the mass of the fiber. [Pg.144]

Not all of the strength and stiffness advantages of fiber-reinforced composite materials can be transformed directly into structural advantages. Prominent among the reasons for this statement is the fact that the joints for members made of composite materials are typically more bulky than those for metal parts. These relative inefficiencies are being studied because they obviously affect the cost trade-offs for application of composite materials. Other limitations will be discussed subsequently. [Pg.31]

Laminated plates are one of the simplest and most widespread practical applications of composite laminates. Laminated beams are, of course, simpler. However, such essentially one-dimensional structural elements do not display well the unique two-dimensional capabilities and characteristics of composite laminates. [Pg.277]

M. J. Salkind, VTOL Aircraft, in Applications of Composite Materials, Michael J. Salkind and Geoffry S. Hollister (Editors), ASTM STP 524, American Society for Testing and Materials, 1973, pp. 76-107 (reprinted with permission). [Pg.362]

Liu J, Zhang Y, Yang T, Ge Y, Zhang S, Chen Z, Gu N (2009) Synthesis, characterization, and application of composite alginate microspheres with magnetic and fluorescent functionalities. J Appl Polym Sci 113 4042 1051... [Pg.227]

The study and application of composite materials are a truly interdisciplinary endeavor that has been enriched by contributions from chemistry, physics, materials science, mechanics and manufacturing engineering. The understanding of the interface (or interphase) in composites is the central point of this interdisciplinary effort. From the early development of composite materials of various nature, the optimization of the interface has been of major importance. While there are many reference books available on composite materials, few of them deal specifically with the science and mechanics of the interface of fiber reinforced composites. Further, many recent advances devoted solely to research in composite interfaces are scattered in different published literature and have yet to be assembled in a readily accessible form. To this end this book is an attempt to bring together recent developments in the field, both from the materials science and mechanics perspective, in a single convenient volume. [Pg.415]

Structural applications of composite materials require not only acceptable static mechanical properites but the ability to withstand the generation and propagation of cracks without premature failre. For example, impact resistance, fracture toughness and fatigue resistance are desireable composite properties. Fiber-matrix structure at the interphase can affect the values attainable for these properties. [Pg.23]

The foregoing summary of applications of composites theory to polymers does not claim to be complete. There are many instances in the literature of the use of bounds, either the Voigt and Reuss or the Hashin-Shtrikman, of simplified schemes such as the Halpin-Tsai formulation84, of simple models such as the shear lag or the two phase block and of the well-known Takayanagi models. The points we wish to emphasize are as follows. [Pg.111]

Application of composite electrodes in the arc discharge process is a well-known route to metallofullerenes [1], To prepare electrodes, a graphite rod is used to be coaxially drilled, stuffed with mixture of metal oxide, graphite powder and thermosetting resin then annealed under vacuum at ca. 2000°C. Such procedure seems to be laborious whereas the yield of metallofullerenes is low [2]. To increase the yield, composite electrodes structure was varied [2] and new equipment was... [Pg.830]

Sebesta F. and John J., An Overview of the Development, Testing, and Application of Composite Absorbers , LA-I2875-MS 1995. [Pg.378]

Development and application of composites containing nanostructured forms of metals open new horizons in creation of novel composite materials with controlled-quality properties and their usage in various kinds of human activity medicine, nanophotonics, catalytic chemical and refining processes, membrane technology, ecology, climate-monitoring systems, pure energetic, etc. [Pg.402]

The interest in multicomponent materials, in the past, has led to many attempts to relate their mechanical behaviour to that of the constituent phases (Hull, 1981). Several theoretical developments have concentrated on the study of the elastic moduli of two-component systems (Arridge, 1975 Peterlin, 1973). Specifically, the application of composite theories to relationships between elastic modulus and microstructure applies for semicrystalline polymers exhibiting distinct crystalline and amorphous phases (Andrews, 1974). Furthermore, as discussed in Chapter 4, the elastic modulus has been shown to be correlated to microhardness for lamellar PE. In addition, H has been shown to be a property that describes a semicrystalline polymer as a composite material consisting of stiff (crystals) and soft, compliant elements. Application of this concept to lamellar PE involves, however, certain difficulties. This material has a microstructure that requires specific methods of analysis involving the calculation of the volume fraction of crystallized material, crystal shape and dimensions, etc. (Balta Calleja et al, 1981). [Pg.127]

Strength and most important commercial fillers for a particular polymer have a lower reduction in these properties at a given volume fraction than other fillers. The applications of composites that depend primarily on mechanical property specifications are too numerous to list some examples are airplane and automotive components. Other important mechanical properties that often justify the use of a filled system vs. one without a filler are abrasion resistance, for instance, automobile tires and resistance to creep, e.g., weightbearing structural components. [Pg.2319]

We start our exposition of the application of composition and inversion to schema evolution, by considering first a relatively simple example of schema evolution. For this section, we will refer to the schema evolution scenario that is graphically illustrated in Fig. 7.2. [Pg.198]

Example 3 Composite pulses are designed to overcome the imperfections of "ideal hard pulses". The Bloch simulator is a suitable tool to illustrate the superiority of a composite 180° pulse inversion compared to a standard 180° pulse. The application of composite pulses in decoupling techniques is discussed in sections 5.3.2 and 5.5.3. In Check it 4.3.4.3 the composite 180° pulse 90x/180y/90x (the indices x and y denote the pulse phase) is demonstrated. These simulations reveal how effective a composite 180° inversion pulse is for different rf offsets. [Pg.174]

Since Fe-Al-Cr alloys with high concentrations of chromium and aluminium cannot easily be manufactured by conventional metal working, the application of composite materials should be considered. An experiment carried out at VOEST-ALPINE GmbH, Linz, has shown, that conventional boiler steels (17CrMo44) can successfully be cladded with Fe-A110-Cr2 by hot rolling. [Pg.219]

Application of composite fullerene membranes for ventilation-filtration systems... [Pg.599]

The first all-around automobile application of composite leaf-springs was made in the Sherpa 200 series van and mini buses built by Freight Rover. These fiber-reinforced plastic (FRP) components for high stress, high-temperature uses were developed by GKN. ICl s Verton, a long-fiber reinforced thermoplastic is also suitable for such applications. [Pg.772]

Within the aerospace industry, advanced composites are used to greatest extent in military aircraft. Commercial aircraft such as the Boeing 757 and 767 contain less than 5% advanced composites by weight, while military aircraft like the GA-18A contain 10%-20%. Typical applications of composites include aircraft wings, tail sections, pressure vessels, and seat rails. [Pg.775]


See other pages where Applications of composites is mentioned: [Pg.270]    [Pg.1]    [Pg.32]    [Pg.37]    [Pg.40]    [Pg.50]    [Pg.221]    [Pg.169]    [Pg.209]    [Pg.84]    [Pg.75]    [Pg.244]    [Pg.37]    [Pg.11]    [Pg.209]    [Pg.243]    [Pg.252]    [Pg.479]    [Pg.539]    [Pg.72]    [Pg.193]    [Pg.264]    [Pg.622]    [Pg.656]    [Pg.1407]   
See also in sourсe #XX -- [ Pg.262 ]

See also in sourсe #XX -- [ Pg.168 , Pg.207 , Pg.217 ]




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