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Pressure level difference

If the sound pressure level difference between the maximum and minimum sound pressure is used, the normal incidence absorption coefficient can be obtained by ... [Pg.118]

Write a general implicit program for transient compressible liquids and gases, taking constant spatial meshes for simplicity. For both flows, assume an initially hydrostatic reservoir, with the sandface suddenly exposed to a prescribed pressure level different from hydrostatic. Run the simulations to steady-state and monitor the flow rate history at the well. Show that the asymptotic results agree with the three complementary steady flow formulations amd solutions given in this chapter. [Pg.121]

I oise Transmission Reduction in HVACSystems. One common use of sound-absorbing treatment is to reduce noise transmission in heating, ventilating, and air-conditioning (HVAC) systems (6). The treatments ate used to reduce the transmission of fan noise and air turbulence noise through ducts into occupied spaces. Noise transmission reduction in duct systems is described in terms of insertion loss, the difference in sound power level or sound pressure level measured at a given location before and after installation of the treatment or sound attenuation, the reduction in sound power between two locations affected by a sound source. The units ate decibels. [Pg.313]

Noise reduction (AIR) is the difference in the average sound pressure level between the source room and the receiving room. When the receiving room is relatively reverberant and the measurements are made in the reverberant fields of the two rooms the relationship between TL and AIR is as follows, where S is the surface area of the sound barrier between the two rooms and is the amount of sound absorption in the receiving room (7). [Pg.315]

The optimum pressure level for gaseous diffusion operation is also determined by comparison at some pressure level the decrease ia equipment size and volume to be expected from increasing the pressure and density is outweighed by the losses that occur ia the barrier efficiency. Nevertheless, because it is weU known that the cost of power constitutes a large part of the total cost of operation of gaseous diffusion plants, it can perhaps be assumed that a practical value of r does not differ gready from the above optimum. Inclusion of this value ia the preceding equations yields... [Pg.87]

The two principal elements of evaporator control are evaporation rate a.ndproduct concentration. Evaporation rate in single- and multiple-effect evaporators is usually achieved by steam-flow control. Conventional-control instrumentation is used (see Sec. 22), with the added precaution that pressure drop across meter and control valve, which reduces temperature difference available for heat transfer, not be excessive when maximum capacity is desired. Capacity control of thermocompression evaporators depends on the type of compressor positive-displacement compressors can utilize speed control or variations in operating pressure level. Centrifugal machines normally utihze adjustable inlet-guide vanes. Steam jets may have an adjustable spindle in the high-pressure orifice or be arranged as multiple jets that can individually be cut out of the system. [Pg.1148]

Sidestream compressors are used in refrigeration processes where, for economy, the refrigerant is flashed off at different pressure levels. Ideally, separate compressors could be used to successively compress the gas back up to the condensing pressure level. The pressure ratio for each stage is low enough to enable this to be done with only one or two impellers in each section. Because of this, compressors can be made with all sections in one casing so that mixing of the streams takes place intern.ll I v. [Pg.423]

As an alternative to the above Eq. (9.167), it is easier to add to the higher pressure level a term depending on the difference between the considered levels, as shown in Table 9.15. [Pg.796]

TABLE 9.15 Coefficients for the Composition of Pressure Levels of Different Sources or of Different Frequencies of the Same Source... [Pg.796]

It is important to quantify the sound pressure levels in dB generated by each source and for each frequency (31.5-8000 Hz) in order to establish which noise will be masked or prevalent. It must be noted that when the pressure levels of two noises differ by more than 10 dB, the resulting level is equal to that of the higher-level source in other words, the noise at the higher level masks the noise at the lower level, which will not be perceptible to the listener (or the phonometer). In this case it is useless to reduce the latter noise, as the composed noise will remain the same, being influenced by the higher-level noise only. [Pg.797]

When the noise transmission takes place in a free field (no reflective surfaces), it is possible to calculate the pressure levels at different distances from the source. For spherical propagation, the following formula can be used ... [Pg.798]

As regards the noise spectrum, the different situations can be analyzed ap proximately with NC (noise criterion) and NR (noise rating) curves (Fig. 9.6.3). NC and NR curves define the octave band limits of an acceptable back ground noise each of them is characterized by a number representing the sound pressure level at 1000 Hz. [Pg.800]

Newby et al. found that increasing the PO turbine pressure resulted in higher steam flow (for a given pinch point temperature difference in the HRSG), increased PO turbine power and overall plant efficiency. However, at the highest pressure of 100 bar attempts to increase the steam flow further resulted in incomplete combustion in the main combustor and the overall thermal efficiency did not increase substantially at this pressure level. [Pg.157]

Harvey et al. gave a parametric calculation of the thermal efficiency of this plant, as a function of turbine inlet temperature, the reformer pinch point temperature difference and the pressure level in the reformer (the compressor overall pressure ratio, r). [Pg.157]

Noise from a compressor plant arises at different sources, and each source has its own pattern of sound pressure levels. Noise levels can be divided into two groups, the low-frequency pulsating air intake sound and the higher-frequency machine noise from compressor, prime mover and fans. Local statutory regulations on noise levels should be determined, and action taken by the supplier to ensure that the noise levels do not exceed those stipulated. [Pg.547]

G. A. White I cannot give you a figure offhand. It depends on so many things, and I am sure you can appreciate that. For example, what methane content do you have in your gas What pressure level do you really want There are many factors involved in establishing a cost difference between atmospheric pressure and 300 lb and 600 lb. There is no way that I can give you an off-the-cuff answer. If you are serious about it, we would be very happy to give you an opinion on a specific set of conditions. But there is no generalization that I can make. [Pg.178]

The pressure profiles obtained from isothermal runs at five different temperatures using this method are shown in Figure 2. It can be observed that in general, the pressure rise is fairly linear for most of the duration of the experiments so that a zero-order approximation may be used to fit the data. This linearity was found to hold even after 5 days for the 175 °C isotherm, reaching a pressure level of approximately 300 psia (this was the longest duration of all the experiments). In the case of the 225 °C isotherm, the pressure accumulation finally levels off at approximately 1100 psia after one day. [Pg.432]

Thus, in equilibrium the level surfaces of the potential serve as surfaces of equal pressure this is not surprising because the potential of the gravitational field and pressure may differ by a constant only. Inasmuch as the force f and grad 5 are parallel to each other then we have... [Pg.144]

Measurements of filtration rates should be repeated at different pressures or different vacuum levels. This gives information on the influence of pressure on the specific cake resistance. The specific resistance of cakes that are difficult to filter is often pressure-dependent. Thus, use of excessive pressure can result in blocking of the cake, causing filtration to stop. In the case of compressible cakes, information is needed over the whole range of pressures being considered for industrial filters since extrapolation of compressibility beyond the experimentally covered region is always risky. The larger the scale of an experimental filter, the less risky predictions based on the experimental data. [Pg.245]

Most process heating is provided from the distribution of steam around sites at various pressure levels. Normally, two or three steam mains will distribute steam at different pressures around the site. The steam system is not only important from the point of view of process heating but is also used to generate a significant amount of power on the site. [Pg.507]

Pressure level. The choice of pressure level for the mixed refrigerant evaporation affects the temperature difference between the process cooling curve and refrigerant evaporation curve. Increasing the overall temperature difference will increase the refrigeration power requirements. [Pg.543]

The effect of pressure on the FTS was studied, according to Table 13.1, at three different pressure levels (8, 20, and 25 bar), keeping constant the other operating conditions at the level of the standard test (T = 230°C, H2/CO inlet molar ratio = 2.1, GHSV = 5,000 cm3 (STP)/h/gcat). [Pg.300]

The mercury level difference equals the difference in pressure between the container and the atmosphere. This mercury level difference is... [Pg.115]

In Fig. 12, we show the computed values of bubble radius for superheated liquid propane at two pressure levels 1 and 5 atm. Consider the inertial rate first. At 1 atm, liquid superheated propane attains the limit of superheat at about 328 K, where the vapor pressure is —18.9 atm. With Eq. (12), Tinertiai 52f m, where t is in seconds. At 5 atm, the driving force [Eyp(To) - Eq] is less than that at 1 atm, but the difference is slight. Thus, the 1 and 5 atm radii are shown as a single line in Fig. 12. [Pg.192]

Feser et al. [214] used a radial flow apparatus to determine the viscous in-plane permeability of differenf DLs af various levels of compression (see Figure 4.26). A stack of round-shaped samples, wifh each layer of material separated with a brass shim, was placed inside two plates. Thicker shim stock was also used in order to control the total thickness of the stack of samples. Compressed air entered fhe apparafus fhrough the upper plate and was forced through the samples in the in-plane direction. After this, the air left the system and flowed through a pressure gage and a rotameter in order to measure the pressure drop and the air flow rate. The whole apparatus was compressed using a hydraulic press for each compression pressure, 10 different flow rates were used. [Pg.263]


See other pages where Pressure level difference is mentioned: [Pg.1097]    [Pg.1097]    [Pg.789]    [Pg.15]    [Pg.405]    [Pg.85]    [Pg.321]    [Pg.796]    [Pg.796]    [Pg.1488]    [Pg.40]    [Pg.183]    [Pg.249]    [Pg.109]    [Pg.543]    [Pg.543]    [Pg.544]    [Pg.651]    [Pg.304]    [Pg.185]    [Pg.94]    [Pg.22]    [Pg.111]    [Pg.206]    [Pg.234]    [Pg.341]   
See also in sourсe #XX -- [ Pg.36 ]




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