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Pressure, changes

Figure 3.8 Separation of a minimum boiling azeotrope by pressure change. (From Holland, Gallun, and Lockett, Chemical Engineering, March 23, 1981, 88 185-200 reproduced by permission.)... Figure 3.8 Separation of a minimum boiling azeotrope by pressure change. (From Holland, Gallun, and Lockett, Chemical Engineering, March 23, 1981, 88 185-200 reproduced by permission.)...
The problem with using a pressure change is that the smaller the change in azeotropic composition, the larger is the recycle in Figs. 3.86 and 3.96. If the azeotrope is not sensitive to changes in pressure, then an extraneous material can be added to the distilla-... [Pg.80]

If an azeotropic mixture is to be separated by distillation, then use of pressure change to alter the azeotropic composition should be considered before use of an extraneous mass-separating agent. Avoiding the use of extraneous materials often can prevent environmental problems later in the design. [Pg.92]

Reservoir fluid sampling is usually done early in the field life in order to use the results in the evaluation of the field and in the process facilities design. Once the field has been produced and the reservoir pressure changes, the fluid properties will change as described in the previous section. Early sampling is therefore an opportunity to collect unaltered fluid samples. [Pg.112]

In abnormally pressured reservoirs, the continuous pressure-depth relationship is interrupted by a sealing layer, below which the pressure changes. If the pressure below the seal is higher than the normal (or hydrostatic) pressure the reservoir is termed overpressured. Extrapolation of the fluid gradient in the overpressured reservoir back to the surface datum would show a pressure greater than one atmosphere. The actual value by which the extrapolated pressure exceeds one atmosphere defines the level of overpressure in the reservoir. Similarly, an underpressured reservoir shows an pressure less than one atmosphere when extrapolated back to the surface datum. [Pg.118]

The vessel was connected to an oil hydraulics apparatus providing a cyclical pressure change of adjustable amplitude and frequency. [Pg.408]

The experimental activity was carried out on a cylindrical pressure vessel whose capacity is 50 litres and made from steel 3 mm thick. Fig. 2 shows the layout of the pressure vessel considered. The pressure vessel was connected to an oil hydraulics apparatus providing a cyclical pressure change of arbitrary amplitude and frequency (fig.3). Furthermore the vessel was equipped with a pressure transducer and some rosetta strain gauges to measure the stresses on the shell and heads. A layout of the rosetta strain gauges locations is shown in fig.4. [Pg.410]

Figure 6. Correlation images of manufactured pipe with defect, under pressure changes of (a) 20psi, (b) 30psi and (e) 40psi. The sealing rule lies to the left of the pipe and the defect zone is highlighted by the white arrow. Figure 6. Correlation images of manufactured pipe with defect, under pressure changes of (a) 20psi, (b) 30psi and (e) 40psi. The sealing rule lies to the left of the pipe and the defect zone is highlighted by the white arrow.
For such a process the pressure p of the surroundings remains constant and is equal to that of the system in its initial and final states. (If there are transient pressure changes within the system, they do not cause changes in the surroundings.) One may then write... [Pg.345]

It is seen that the pressure variation tends to zero when - , so In coarsely porous pellets with high permeability the pressure change Induced by reaction may be very small compared t/ith the absolute pressure. In this sense, then, the pellet approaches an isobaric system at high values of the permeability. [Pg.132]

This quantity has been measured directly to be 0.016 K atm Note that a pressure change of 60 atm is needed to change Tg by 1 K. [Pg.247]

Flow Past Bodies. A fluid moving past a surface of a soHd exerts a drag force on the soHd. This force is usually manifested as a drop in pressure in the fluid. Locally, at the surface, the pressure loss stems from the stresses exerted by the fluid on the surface and the equal and opposite stresses exerted by the surface on the fluid. Both shear stresses and normal stresses can contribute their relative importance depends on the shape of the body and the relationship of fluid inertia to the viscous stresses, commonly expressed as a dimensionless number called the Reynolds number (R ), EHp/]1. The character of the flow affects the drag as well as the heat and mass transfer to the surface. Flows around bodies and their associated pressure changes are important. [Pg.89]

Further reductions in reservoir pressure move the shock front downstream until it reaches the outlet of the no22le E. If the reservoir pressure is reduced further, the shock front is displaced to the end of the tube, and is replaced by an obflque shock, F, no pressure change, G, or an expansion fan, H, at the tube exit. Flow is now thermodynamically reversible all the way to the tube exit and is supersonic in the tube. In practice, frictional losses limit the length of the tube in which supersonic flow can be obtained to no more than 100 pipe diameters. [Pg.95]

Averaging the velocity using equation 50 yields the weU-known Hagen-Poiseuille equation (see eq. 32) for laminar flow of Newtonian fluids in tubes. The momentum balance can also be used to describe the pressure changes at a sudden expansion in turbulent flow (Fig. 21b). The control surface 2 is taken to be sufficiently far downstream that the flow is uniform but sufficiently close to surface 3 that wall shear is negligible. The additional important assumption is made that the pressure is uniform on surface 3. The conservation equations are then applied as follows ... [Pg.108]

Fig. 4. Plot of maximum rate of pressure change for propane VPO showing NTC region 5.33 kPa propane, 13.33 kPa O2. Courtesy of Blackwell Scientific... Fig. 4. Plot of maximum rate of pressure change for propane VPO showing NTC region 5.33 kPa propane, 13.33 kPa O2. Courtesy of Blackwell Scientific...
The minienvironment approach to contamination control has been increasing in use. A minienvironment is a localized environment created by an enclosure that isolates the product wafer from contamination and people (48). Another approach is using integrated processing, where consecutive processes are linked in a controlled environment (32). Both requite in situ sensors (qv) to measure internal chamber temperatures, background contamination, gas flow rates, pressure changes, and particularly wafer temperature (4). [Pg.355]

Ozone can be analyzed by titrimetry, direct and colorimetric spectrometry, amperometry, oxidation—reduction potential (ORP), chemiluminescence, calorimetry, thermal conductivity, and isothermal pressure change on decomposition. The last three methods ate not frequently employed. Proper measurement of ozone in water requites an awareness of its reactivity, instabiUty, volatility, and the potential effect of interfering substances. To eliminate interferences, ozone sometimes is sparged out of solution by using an inert gas for analysis in the gas phase or on reabsorption in a clean solution. Historically, the most common analytical procedure has been the iodometric method in which gaseous ozone is absorbed by aqueous KI. [Pg.503]

Likewise, the microscopic heat-transfer term takes accepted empirical correlations for pure-component pool boiling and adds corrections for mass-transfer and convection effects on the driving forces present in pool boiling. In addition to dependence on the usual physical properties, the extent of superheat, the saturation pressure change related to the superheat, and a suppression factor relating mixture behavior to equivalent pure-component heat-transfer coefficients are correlating functions. [Pg.96]

Fig. 28. Cycle of 34-ceU regenerative hydrogen—oxygen fuel cell where A represents the charging region at 10 A, B represents discharging at 18.2 A. Both (—) voltage and (—) pressure changes are shown. To convert MPa to psig, multiply by 145. Fig. 28. Cycle of 34-ceU regenerative hydrogen—oxygen fuel cell where A represents the charging region at 10 A, B represents discharging at 18.2 A. Both (—) voltage and (—) pressure changes are shown. To convert MPa to psig, multiply by 145.
By applying the conservation equations of mass and energy and by neglecting the small pressure changes across the flame, the thickness of the preheating and reaction 2ones can be calculated for a one-dimensional flame (1). [Pg.518]

Most theories of droplet combustion assume a spherical, symmetrical droplet surrounded by a spherical flame, for which the radii of the droplet and the flame are denoted by and respectively. The flame is supported by the fuel diffusing from the droplet surface and the oxidant from the outside. The heat produced in the combustion zone ensures evaporation of the droplet and consequently the fuel supply. Other assumptions that further restrict the model include (/) the rate of chemical reaction is much higher than the rate of diffusion and hence the reaction is completed in a flame front of infinitesimal thickness (2) the droplet is made up of pure Hquid fuel (J) the composition of the ambient atmosphere far away from the droplet is constant and does not depend on the combustion process (4) combustion occurs under steady-state conditions (5) the surface temperature of the droplet is close or equal to the boiling point of the Hquid and (6) the effects of radiation, thermodiffusion, and radial pressure changes are negligible. [Pg.520]

For the liquid-phase mass-transfer coefficient /cl, the effects of total system pressure can be ignored for all practical purposes. Thus, when using Kq and /cl for the design of gas absorbers or strippers, the primary pressure effects to consider will be those which affect the equilibrium curves and the values of m. If the pressure changes affect the hydrodynamics, then Icq, and a can all change significantly. [Pg.610]


See other pages where Pressure, changes is mentioned: [Pg.1]    [Pg.256]    [Pg.345]    [Pg.403]    [Pg.288]    [Pg.190]    [Pg.684]    [Pg.647]    [Pg.281]    [Pg.354]    [Pg.64]    [Pg.91]    [Pg.110]    [Pg.511]    [Pg.209]    [Pg.21]    [Pg.22]    [Pg.24]    [Pg.451]    [Pg.309]    [Pg.478]    [Pg.562]    [Pg.648]    [Pg.655]    [Pg.760]    [Pg.763]    [Pg.765]    [Pg.788]   
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See also in sourсe #XX -- [ Pg.208 ]

See also in sourсe #XX -- [ Pg.336 , Pg.391 , Pg.620 ]

See also in sourсe #XX -- [ Pg.208 ]

See also in sourсe #XX -- [ Pg.445 ]




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