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Flexure Bending Stress

HV measurement of bulk nano-twinned cubic boron nitride (henceforth nt-cBN) samples with a standard square-pyramidal diamond indenter is shown in Fig. 9.19. An explanation of the connection between this figure and observations of the inverse H-P effect are found below. Reliable hardness values are best determined from the asymptotic hardness region. In Fig. 9.19, the variations in Vickers hardness are recorded by applying a series of loads. The asymptotic hardness value obtained at loads above 3 N was extremely high, 108 GPa, which [Pg.716]

An inverse H-P phenomenon has been observed by researchers in various metals and also in some ceramics, e.g., in boron nitride. Attempts to explain this phenomenon have been made, though some claim that it is not a real characteristic (perhaps even a sort of artifact). Recent studies tend to indicate that the inverse H-P effect is real, true and apparently universal. However, the debate is now focused on its mechanism. Explanations do exist suggesting various mechanisms that may be responsible for this effect [7], even that of twinning (e.g., Tian et al. [32]). At these small nanosizes, dislocations cannot be the cause of this observed mechanical behavior, since such extended defects have certain dimensions that cannot be accommodated within the space of low range nanograins dislocations are unlikely to reside in such miniscule structures. As stated above, in nanoscale materials, GBS is the likely mechanism affecting behavior. In Fig. 9.20, a Vickers indentation is shown for a nanocrystalline cBN, as a function of crystallite size. Here, ABNNC stands for aggregated boron nitride nanocomposite . [Pg.718]

The continuous hardening behavior with decreasing microstmctural sizes, down to 3.8 nm in cBN, may be explained as follows. For nano-twins with thicknesses [Pg.719]

Hhp = (Hq + kd ) and Hqc = (Cd ) represent dislocation-related dislocation hardening based on the H-P effect and bandgap-related hardening based on the quantum confinement effect, as indicated above, following Tse s [34] calculations. Ho is the single-crystal hardness and k is a material constant. C is a material-specific parameter equal to zero for metals and equal to 211Ny exp (1.191fi) for covalent materials, where Ne is the valence electron density and fj is the Philips ionicity of the chemical bond. [Pg.720]

As previously mentioned, some explain the inverse H-P effect by twinning [7]. From the above examples, it may be assumed that, despite the claims of some researchers of the universality of the inverse H-P effect, its validity remains debatable. The above data axe from experiments performed quite recently (2006 and 2012), so this debate is still unresolved. [Pg.721]


Fiber Stress at Proportional Limit. The FSPL is the maximum bending stress a material can sustain under static conditions and still exhibit no permanent set or distortion. It is by definition the amount of unit stress on the y-coordinate at the proportional limit of the material (Figure 2, Point A Figure 6, Point A). FSPL is derived using the flexure formula... [Pg.221]

This analysis combines the primary membrane stress due to pressure with the secondary bending stress resulting from the flexure of the nozzle about the hard axis. [Pg.206]

The flexural creep stiffness at loading time t, S t) [or measured flexural creep stiffness, S ,(r)], is the ratio obtained by dividing the bending stress by the bending strain. [Pg.212]

The flexural creep compliance, D t), if needed to be determined, is the inverse of S (t), that is, the ratio obtained by dividing the bending shear by the bending stress. [Pg.212]

Pipe support configurations are an important facet of design. A small increase in diameter greatly increases the flexural rigidity of a pipe span, which is proportional to d, and therefore increases the permissible support spacing (the load of the fluid content increases only as d. Support considerations are rather different in the case of plastic pipes, which often need full-length support in the smaller sizes to avoid excessive deflection and bending stresses. [Pg.158]

The maximum bending stress Sij in a beam under a bending or flexural load is ... [Pg.117]

In order to evaluate the design flexural resistance of the FRP-strengthened member as well, in the presence of an axial force (combined compressive and bending stress), the principles introduced in the previous chapters are valid, as long as the dependence of the design flexural capacity Mr, of the strengthened member on the normal factored axial force, Nsi, is taken into account. [Pg.70]

One of the main reasons for adding mineral fillers to thermoplastics is to increase the modulus (stiffness). Tensile (under tension) modulus is the ratio of stress to strain, at some low amount of strain, below the elastic limit. Flexural (bending) modulus is also often measured. The most relevant modulus to measure depends upon the expected deformation mode of the part that will be made from the material. Often, the flexural modulus and tensile modulus are rather similar. The exception is the case of anisotropic fillers, which can become aligned in the flow direction when the test specimens are moulded. [Pg.372]

As can be seen from Table 6.5, with the increase of calcium carbonate whiskers, the flexural strengths of the composites increase first and then decrease. When the whisker filling content is 5%-10%, the bending stress of the composite material increases 11.5% over that of pure PP. In addition, the bending fracture strains of composite materials filled with whiskers... [Pg.262]

As explained previously by Lu et al. [215], there are standard testing methods and equipment that can be employed for reinforced aerogel materiak such as polymer cross-linked ones (X-aerogek), although their standard mechanical characterization does not exist. Flexural tests are carried out in three-point bending mode, normally leading to failure imder tensile bending stresses in... [Pg.551]

Bending stress or flexural stress commonly occurs in two instances, shown in Fig. 1.5. One is called a simply supported structural beam bending and the other is called cantilever bending. For the simply supported structural beam, the upper surface of the bending beam is in compression and the bottom surface is in tension. The neutral axis (NA) is a region of zero stress. The bending stress (bending moment, which... [Pg.2]

Simply supported beam bending Figure 1.5 Illustration of flexural or bending stress. [Pg.2]


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Bending stresses

Flexural stress

Flexure

Stress, types three-point flexural/bending test

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