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Velocity-change experiment

Both ultrasonic and radiographic techniques have shown appHcations which ate useful in determining residual stresses (27,28,33,34). Ultrasonic techniques use the acoustoelastic effect where the ultrasonic wave velocity changes with stress. The x-ray diffraction (xrd) method uses Bragg s law of diffraction of crystallographic planes to experimentally determine the strain in a material. The result is used to calculate the stress. As of this writing, whereas xrd equipment has been developed to where the technique may be conveniently appHed in the field, convenient ultrasonic stress measurement equipment has not. This latter technique has shown an abiHty to differentiate between stress reHeved and nonstress reHeved welds in laboratory experiments. [Pg.130]

Judging by these results the angular momentum relaxation in a dense medium has the form of damped oscillations of frequency jRo = (Rctc/to)i and decay decrement 1/(2tc). This conclusion is quantitatively verified by computer experiments [45, 54, 55]. Most of them were concerned with calculations of the autocorrelation function of the translational velocity v(t). However the relation between v(t) and the force F t) acting during collisions is the same as that between e> = J/I and M. Therefore, the results are qualitatively similar. In Fig. 1.8 we show the correlation functions of the velocity and force for the liquid state density. Oscillations are clearly seen, which point to a regular character of collisions and non-Markovian nature of velocity changes. [Pg.35]

Fig. 1.19 Spin-echo based pulse sequence to each gradient pulse, A the separation between encode velocity change. The gradients are each pair of bipolar gradient pulses and tm the stepped pair-wise independently (2D VEXSY) mixing time between the bipolar gradient pairs, or simultaneously (1 D VEXSY). For a VEXSY The opposite polarity of the bipolar gradient experiment, 7q to k4 are usually applied along pair is realized by an inversion 180° pulse, the same spatial direction. 8 is the duration of... Fig. 1.19 Spin-echo based pulse sequence to each gradient pulse, A the separation between encode velocity change. The gradients are each pair of bipolar gradient pulses and tm the stepped pair-wise independently (2D VEXSY) mixing time between the bipolar gradient pairs, or simultaneously (1 D VEXSY). For a VEXSY The opposite polarity of the bipolar gradient experiment, 7q to k4 are usually applied along pair is realized by an inversion 180° pulse, the same spatial direction. 8 is the duration of...
Fig. 4.6.7 Projections along the secondary diagonal from the 2D VEXSY experiments presented partly in Figure 4.6.5 and 4.6.6. (a) Distribution of velocity change obtained among others from Figure 4.6.5 (a, d) of the SMC module, (b) Distribution of velocity change obtained among others from Figure 4.6.6(a, d) of the SPAN module, (c) Three out of six distributions presented in (a) and (b) are displayed as the distribution of acceleration, which is obtained by dividing the velocity... Fig. 4.6.7 Projections along the secondary diagonal from the 2D VEXSY experiments presented partly in Figure 4.6.5 and 4.6.6. (a) Distribution of velocity change obtained among others from Figure 4.6.5 (a, d) of the SMC module, (b) Distribution of velocity change obtained among others from Figure 4.6.6(a, d) of the SPAN module, (c) Three out of six distributions presented in (a) and (b) are displayed as the distribution of acceleration, which is obtained by dividing the velocity...
Figure 5.11 A constant velocity Mossbauer experiment reveals the kinetics of the denitridation of an iron nitride in different gases at 525 K. The negative part of the time scale gives the transmission of the most intense peak of the nitride at time zero the gas atmosphere is changed to the desired gas. Denitridation occurs relatively fast in H2, but is retarded by CO, whereas the nitride is stable in an inert gas such as helium (from Hummel etal. [33]). Figure 5.11 A constant velocity Mossbauer experiment reveals the kinetics of the denitridation of an iron nitride in different gases at 525 K. The negative part of the time scale gives the transmission of the most intense peak of the nitride at time zero the gas atmosphere is changed to the desired gas. Denitridation occurs relatively fast in H2, but is retarded by CO, whereas the nitride is stable in an inert gas such as helium (from Hummel etal. [33]).
The locus of a fully developed velocity change with height from the new point source as the wind moves downstream is called the boundary layer. Above this layer the effect of the change in roughness has not been completed. It appears from experiments that the boundary layer increases rather slowly in thickness as the wind moves downstream from the new obstacle. Some recent data show that the thickness at any given distance is proportional to the change in surface roughness and is independent of velocity. [Pg.402]

The definition of q and the displacement R in Fig. 5.4.5 in terms of a position-change experiment performed in 2D space can be carried one step further having identified qv = 9 as the Fourier-conjugate variable of average velocity R/z in (5.4.28), a... [Pg.195]

In velocity-change NMR the variables q and q 2 replace the axes ki and kz in Fig. 5.4.5, and ui and V2 replace r and r2 (Fig. 5.4.12). In a coordinate frame rotated by 45° the difference coordinate corresponds to acceleration a and the other to velocity v, so that this exchange experiment can be read as a velocity-acceleration correlation experiment. Following the coordinate transformations (5.4.21) for position-change spectroscopy, the following coordinate transformations apply for velocity-change spectroscopy. [Pg.196]

Recently MAQO experiments have also been performed for the Kondo lattice compound CePbj, see Niki et al. (1987). Figure 43 shows relative velocity changes for the c - Cj2 mode for B k in the temperature range between 0.38 K to 1.7 K. For magnetic fields from 18-23 T a clear MAQO with frequency F = 617 T is observed with an effective mass m lm = 43. More extensive experiments have to be performed in order to determine the Fermi surface geometry. The complicated B-T phase diagram will be discussed in sect. 4. [Pg.298]

Our studies of the effect of velocity-changing collisions in an rf-laser double resonance experiment contribute to a new vista into the role of collisictis in laser spectroscopy of sub-level structures the limitation of the observation time of the active atoms due to narrow-bandwidth optical excitation and simultaneous velocity diffusion can be of importance for a variety of spectroscopic techniques that use a velocity-selective excitation and detection of either sublevel populations or sublevel coherence. On the other hand, the collisional velocity diffusion of sublevel coherence within an optical Doppler distribution can also give rise to new and surprising phenomena as will discussed in the next section. [Pg.181]

The velocity gradient Av/d is a measure of the rate with which velocity changes with distance and it measures the shearing that the fluid experiences. The term is often called the rate of shear . The force per unit area that is required for the maintenance of the shearing action, FI A, is known as the shear stress. A stress is a force per unit area and has the same units as pressure. [Pg.53]

In this test, a metal sample is rotated in the solution. A rotating cylinder is used to simphfy fluid dynamics equations so that corrosion rate can be correlated with shear stress or mass transfer, which in turn can be related to velocity effects in piping and equipment. The same electn> chemical techniques used on static samples are applicable to the rotating cylinder electrode. By coupling the samples to electrochemical measirring equipment, one can measure qualitatively the effects of stepped velocity changes in one experiment. [Pg.789]

The teacher then confirmed you need to have another definition of the efficiency and wrote e = AEtask / AEsouroe on the blackboard, a definition that they had used before. Students then immediately came up with proposals for measuring the velocity change of the flywheel, and the temperature change and heat capacity of the hot reservoir. This completed students design of an experiment that would test their predictions. [Pg.306]

All flowing fluids experience shear, which arises from the way in which the velocity of the fluid increases as the distance from the stationary surface over which it is flowing increases. For flow in pipes, this is the distance (y) from the inside edge of the pipe wall. (See Figs. 48.5a and b.) The rate at which the velocity changes with respect to distance from the pipe wall is called the shear rate (y), and is measured in reciprocal seconds, s i (where [ft/s]/ft = s ). [Pg.632]

In Fig. 6.47, the calculated change of velocity with porosity is compared with the experimental results from Han et al. (1986) in Fig. 6.10. For a direct comparison, the velocities from experiments are converted to dry status by Gassmann s equation. Clean and shaly sandstone shows different values for Vi and for the ratio oCpore/agrain-... [Pg.246]

Many combustion-related experiments as well as practical devices involve reaction in flowing gas streams. When reacting gas is moving, the kinetic energy of motion must be considered as part of the total energy that is conserved when chemical reaction releases heat energy. In essence, the flow velocity changes when reaction occurs. The differential equations that we use to describe the process must take this into account. [Pg.13]


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