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Load and Shear

In three commonly used modes, the top layers are driven  [Pg.83]

Pulling with a spring, e.g., Fx = —k[X — X0(t)], where Fx is the force acting on the top layer in the x direction, k reflects the (effective) stiffness of the driving device, and Xo(/) denotes the position of the driving device as a function of time. [Pg.83]

The typical choices for the predefined trajectories or forces are constant velocity, including zero velocity, constant separation, constant forces, and/or [Pg.83]

It is often beneficial to define a coordinate Rti that describes the center of mass of the top layer. There are three common ways to set up the top layer. (1) The positions of top layer atoms r are confined to (lattice) sites rW)o, which are connected rigidly to the top layer. (2) The top layer atoms are coupled elastically to sites rra 0 fixed relative to the top layer, e.g., with springs of stiffness k. (3) An effective potential, such as a Steele potential Vs34 is applied between embedded atoms and the top layer. Specific advantages and disadvantages are associated with each method. Approach (1) may be the one that is most easily coded, (2) allows one to thermostat the outermost layer in an effective manner, whereas (3) is probably cheapest in terms of CPU time. [Pg.84]

The force on the top wall Fti is evaluated differently for each driving mode mentioned above. [Pg.84]


Fig. 2.4. Within the elastic range it is possible to relate uniaxial strain data obtained under shock loading to isotropic (hydrostatic) loading and shear stress. Such relationships can only be calculated if elastic constants are not changed with the finite amplitude stresses. Fig. 2.4. Within the elastic range it is possible to relate uniaxial strain data obtained under shock loading to isotropic (hydrostatic) loading and shear stress. Such relationships can only be calculated if elastic constants are not changed with the finite amplitude stresses.
A thorough study, at 20°C, of the deformation of cold drawn Alkathene WNF15 has been published recently by Ladizesky and Ward. Young s moduli and Poisson s ratios were determined from the changes in dimensions under load, and shear moduli using extrapolations from the... [Pg.305]

Posterior compression reduces the bending in the rods and screws. Reduction of the slip reduces the moments in the rods and screws. Anterior cages reduce the shear loading and shear displacements at L5-S1 and thus the bending in the rods and screws. [Pg.49]

Protective sleeves are intended to help shield the pipe at the connection point from bearing loads and shear forces and to limit the maximum pipe bending. [Pg.359]

Historically, Bailey and Courtney-Pratt [176] were the first to combine crossed cylinder mica sheets as molecularly smooth surfaces and FECO for distance measurement in 1955. They used this approach to map out the contact area between mica surfaces at different loads and shear forces. The first SFA was built by Tabor and Winterton in 1968 [30] and subsequently by Tabor and IsraelachviU in 1972 [56]. In 1976, the newly designed SFA Mk 1 by Israelachvili and Adams [55, 177] was introduced that allowed measurements in liquids or vapors. With the SFA Mk 2, an adjustable double-cantilever spring extended the range of measurable forces and an optional friction device [644] allowed to measure shear forces of molecular thin films at defined loads. Between 1985 and 1989 Israelachvili and McGuiggan developed the SFA Mk 31 to overcome several limitations of the SFA Mk 2 [179]. The new system had a more compact design for higher attainable stiffness and lower thermal drift, an improved control system for mechanical movement of surfaces, and was more easy to clean. [Pg.62]

Load bearing capabiUties are dependent upon the adherend, joint design, rate of loading, and temperature. Values given represent the type of adherends normally used at room temperature. Lap shear values approximate those obtainable from an overlap of 3.2 cm. ... [Pg.232]

A significant aspect of hip joint biomechanics is that the stmctural components are not normally subjected to constant loads. Rather, this joint is subject to unique compressive, torsion, tensile, and shear stress, sometimes simultaneously. Maximum loading occurs when the heel strikes down and the toe pushes off in walking. When an implant is in place its abiUty to withstand this repetitive loading is called its fatigue strength. If an implant is placed properly, its load is shared in an anatomically correct fashion with the bone. [Pg.189]

A rotational viscometer connected to a recorder is used. After the sample is loaded and allowed to come to mechanical and thermal equiUbtium, the viscometer is turned on and the rotational speed is increased in steps, starting from the lowest speed. The resultant shear stress is recorded with time. On each speed change the shear stress reaches a maximum value and then decreases exponentially toward an equiUbrium level. The peak shear stress, which is obtained by extrapolating the curve to zero time, and the equiUbrium shear stress are indicative of the viscosity—shear behavior of unsheared and sheared material, respectively. The stress-decay curves are indicative of the time-dependent behavior. A rate constant for the relaxation process can be deterrnined at each shear rate. In addition, zero-time and equiUbrium shear stress values can be used to constmct a hysteresis loop that is similar to that shown in Figure 5, but unlike that plot, is independent of acceleration and time of shear. [Pg.169]

The equations and methods for determining viscosity vary greatly with the type of instmment, but in many cases calculations may be greatly simplified by calibration of the viscometer with a standard fluid, the viscosity of which is known for the conditions involved. General procedures for calibration measurement are given in ASTM D2196. The constant thus obtained is used with stress and shear rate terms to determine viscosity by equation 25, where the stress term may be torque, load, or deflection, and the shear rate may be in rpm, revolutions per second (rps), or s F... [Pg.184]

Adhesives are used to transfer loads and are typically designed with much higher tensile and shear strengths than sealants. The most important rating of an adhesive ia many appHcatioas is the determiaatioa of how much load it can handle. Some sealants are used as adhesives and some adhesives as sealants and thus arises the occasional blurring of their roles. If the material s primary function is the exclusion of wiad, water, dirt, etc, it is a sealant. [Pg.308]

These values are determined by experiment. It is, however, by no means a trivial task to measure the lamina compressive and shear strengths (52,53). Also the failure of the first ply of a laminate does not necessarily coincide with the maximum load that the laminate can sustain. In many practical composite laminates first-ply failure may be accompanied by a very small reduction in the laminate stiffness. Local ply-level failures can reduce the stress-raising effects of notches and enhance fatigue performance (54). [Pg.14]

Samples are most frequently shock deformed under laboratory conditions utilizing either explosive or gun-launched flyer (driver) plates. Given sufficient lateral extent and assembly thickness, a sample may be shocked in a onedimensional strain manner such that the sample experiences concurrently uniaxial-strain loading and unloading. Based on the reproducibility of projectile launch velocity and impact planarity, convenience of use, and ability to perform controlled oblique impact (such as for pressure-shear studies) guns have become the method of choice for many material equation-of-state and shock-recovery studies [21], [22]. [Pg.194]

Variations on the basic lap joint are preferred to give Large contact areas using uniform thin sections. If at all, the joint should be loaded in shear and... [Pg.346]

The critical-speed calculation of a rotating shaft proceeds with equations to relate loads and deflections from station — 1 to station n. The shaft shear V can be computed using the following relationship ... [Pg.196]


See other pages where Load and Shear is mentioned: [Pg.83]    [Pg.652]    [Pg.99]    [Pg.79]    [Pg.123]    [Pg.123]    [Pg.160]    [Pg.197]    [Pg.273]    [Pg.41]    [Pg.156]    [Pg.181]    [Pg.127]    [Pg.92]    [Pg.894]    [Pg.432]    [Pg.615]    [Pg.83]    [Pg.652]    [Pg.99]    [Pg.79]    [Pg.123]    [Pg.123]    [Pg.160]    [Pg.197]    [Pg.273]    [Pg.41]    [Pg.156]    [Pg.181]    [Pg.127]    [Pg.92]    [Pg.894]    [Pg.432]    [Pg.615]    [Pg.325]    [Pg.269]    [Pg.290]    [Pg.250]    [Pg.234]    [Pg.228]    [Pg.513]    [Pg.508]    [Pg.87]    [Pg.273]    [Pg.273]    [Pg.510]    [Pg.51]    [Pg.56]    [Pg.228]    [Pg.290]    [Pg.347]    [Pg.375]    [Pg.145]   


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