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Experimental speed

In this particular example turbine speed control was taking place. The closed loop feedback is turbine speed in rpm as measured by an optical pickup on the generator box (nearly instantaneous). In this test, the experimental speed controller and the simulated speed controller (in both models), used a proportional gain of 0.001 and an integral gain of 0.001 x 0.75 with an input of speed error in rpm and output in fuel valve %. For the experiment presented, the fuel flow rate in grams per second... [Pg.257]

The resulting experimental speed is shown in Fig. 3. Special attention to the electroendosmotic flow will be given later. [Pg.7]

It should be emphasized that although this success of the Debye model has made it a standard starting point for qualitative discussions of solid properties associated with lattice vibrations, it is only a qualitative model with little resemblance to real normal-mode spectra of solids. Figure 4.1 shows the numerically calculated density of modes of lead in comparison with the Debye model for this metal as obtained from the experimental speed of sound. Table 4.1 list the Debye temperature for a few selected solids. [Pg.142]

The Gaussian curves in Fig. 3 (right column) are obtained by fitting the outer two peaks of the experimental speed distributions (corresponding to the FI and SI channels) to Gaussian distributions with the following functional form ... [Pg.53]

It is interesting to compare the ratio of two experimental speeds at each time point, because we obtain, in pseudo-steady state modes, and sometimes only in this case, ratios that are independent of time. This property will be nsed (see section 11.3.1) to verify the pseudo-steady state assumption for a system. We will cany out calculation for the thermogravimetrie and calorimetrie speed ratio. [Pg.387]

Consider again expressions [11.2] and [11.4] for both experimental speeds in pseudo-steady state modes and the ratio ... [Pg.387]

We are going to base our measurement of the two experimental speed ratios on the speed ratio of the mass change and the calorimetric flow. [Pg.388]

The rate (in practice, an experimental speed if the pseudo-steady state mode were already established) is measured at each chosen time point before the switch and after it (Figure 11.3). The duration of a switch mnst be sufficierrtly short so that the space fimction practically does not change dnring this duration (this part is almost hnear on the kinetic curve). [Pg.391]

FIGURE 9.6 Comparison of calculated and experimental speed and temperature profiles for PET. (Reprinted by permission of the publisher from George, 1982.)... [Pg.286]

The experimental speed is usually obtained for closed systems as a function of the concentrations and temperature. Curiously, however, speeds as a function of time or fractional extent are never obtained. At most, the intervention of time appears in some reactions through a notion of cirrrent order that differs from an initial order. Moreover, it is not specified whether the speeds are compared at constant time or fractional extent. [Pg.91]

It is essential for the rotating-disc that the flow remain laminar and, hence, the upper rotational speed of the disc will depend on the Reynolds number and experimental design, which typically is 1000 s or 10,000 rpm. On the lower lunit, 10 s or 100 rpm must be applied in order for the thickness of tlie boundary layer to be comparable to that of the radius of the disc. [Pg.1936]

In all other cases the observed result will depend upon both the speed of mixing and the speed of nitration. The relative rate will be greater than unity by an amount peculiar to the conditions of the experiment. Again, if the alkylbenzene is sufficiently reactive to be nitrated upon encounter, whilst benzene is not, the relative rate will be greater than unity and, for the experimental conditions, will be a limiting upper value no matter what aromatic is used. [Pg.65]

Computer simulation of the reactor kinetic hydrodynamic and transport characteristics reduces dependence on phenomenological representations and idealized models and provides visual representations of reactor performance. Modem quantitative representations of laminar and turbulent flows are combined with finite difference algorithms and other advanced mathematical methods to solve coupled nonlinear differential equations. The speed and reduced cost of computation, and the increased cost of laboratory experimentation, make the former increasingly usehil. [Pg.513]

The second class of grinding equipment is used to prepare dispersions. Typical of this class are baU and pebble mills, ultrasonic mills, and attrition mills. SoHds, eg, sulfur, antioxidants, accelerators, and zinc oxide, are generaUy ground on this equipment (see Size reduction). BaU mill action is assisted in some mills by a combination of dispersion circulation by an external pump and mechanical osciUation of an otherwise fixed nonrotary mill chamber. Where baU mill chambers are rotated it is necessary to experimentally estabHsh an optimum speed of rotation, the size and weight of the baU charge, and ensure the mills do not overheat during the grinding period. [Pg.257]


See other pages where Experimental speed is mentioned: [Pg.74]    [Pg.82]    [Pg.74]    [Pg.421]    [Pg.381]    [Pg.785]    [Pg.122]    [Pg.74]    [Pg.82]    [Pg.74]    [Pg.421]    [Pg.381]    [Pg.785]    [Pg.122]    [Pg.543]    [Pg.362]    [Pg.1481]    [Pg.1744]    [Pg.1904]    [Pg.2123]    [Pg.2254]    [Pg.498]    [Pg.381]    [Pg.632]    [Pg.4]    [Pg.93]    [Pg.685]    [Pg.248]    [Pg.437]    [Pg.83]    [Pg.644]    [Pg.548]    [Pg.16]    [Pg.215]    [Pg.510]    [Pg.515]    [Pg.409]    [Pg.114]    [Pg.214]   
See also in sourсe #XX -- [ Pg.387 ]




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