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Heat of vaporization, liquids

Calculated the vapor flow rate leaving the reboiler for the duty and liquid heat of vaporization. [Pg.907]

P = vapor pressure of liquid heat of vaporization = 5090cal/mole... [Pg.117]

Heat of combustion of die liquid Heat of vaporization of the liquid Boiling point of the liquid Ambient temperature ... [Pg.221]

Enthalpies are referred to the ideal vapor. The enthalpy of the real vapor is found from zero-pressure heat capacities and from the virial equation of state for non-associated species or, for vapors containing highly dimerized vapors (e.g. organic acids), from the chemical theory of vapor imperfections, as discussed in Chapter 3. For pure components, liquid-phase enthalpies (relative to the ideal vapor) are found from differentiation of the zero-pressure standard-state fugacities these, in turn, are determined from vapor-pressure data, from vapor-phase corrections and liquid-phase densities. If good experimental data are used to determine the standard-state fugacity, the derivative gives enthalpies of liquids to nearly the same precision as that obtained with calorimetric data, and provides reliable heats of vaporization. [Pg.82]

Example 9.1 A process involves the use of benzene as a liquid under pressure. The temperature can be varied over a range. Compare the fire and explosion hazards of operating with a liquid process inventory of 1000 kmol at 100 and 150°C based on the theoretical combustion energy resulting from catastrophic failure of the equipment. The normal boiling point of benzene is 80°C, the latent heat of vaporization is 31,000 kJ kmol the specific heat capacity is 150 kJkmoh °C , and the heat of combustion is 3.2 x 10 kJkmok. ... [Pg.269]

Solution The fraction of liquid vaporized on release is calculated from a heat balance. The sensible heat above saturated conditions at atmospheric pressure provides the heat of vaporization. The sensible heat of the superheat is given by... [Pg.269]

Triple point temperature K Heat of fusion kJ/lc Heat of vaporization kJ/kg Liquid conductivity atr, W / (m-K) Liquid conductivity AtT W/(m-I0 Temperature Ti K Temperature h K... [Pg.417]

Triple point temperature Heat of fusion Heat of vaporization Liquid conductivity at r, Liquid conductivity at Temperature Tx Temperature Tz... [Pg.421]

Derive an equation for the heat of vaporization of a liquid as a function of drop radius r. [Pg.93]

On compression, a gaseous phase may condense to a liquid-expanded, L phase via a first-order transition. This transition is difficult to study experimentally because of the small film pressures involved and the need to avoid any impurities [76,193]. There is ample evidence that the transition is clearly first-order there are discontinuities in v-a plots, a latent heat of vaporization associated with the transition and two coexisting phases can be seen. Also, fluctuations in the surface potential [194] in the two phase region indicate two-phase coexistence. The general situation is reminiscent of three-dimensional vapor-liquid condensation and can be treated by the two-dimensional van der Waals equation (Eq. Ill-104) [195] or statistical mechanical models [191]. [Pg.132]

Equation (3.7) gives a simple procedure for evaluating the entropy change accompanying a change of state. At the normal boiling point of a liquid, for example, the heat is absorbed reversibly and equals the heat of vaporization AH,. Since T is constant, the entropy of vaporization is AH,/T. For benzene, for example, AS, = (30.8 k J mol" )/353 = 87 J K mol. ... [Pg.143]

Combustion. The primary reaction carried out in the gas turbine combustion chamber is oxidation of a fuel to release its heat content at constant pressure. Atomized fuel mixed with enough air to form a close-to-stoichiometric mixture is continuously fed into a primary zone. There its heat of formation is released at flame temperatures deterruined by the pressure. The heat content of the fuel is therefore a primary measure of the attainable efficiency of the overall system in terms of fuel consumed per unit of work output. Table 6 fists the net heat content of a number of typical gas turbine fuels. Net rather than gross heat content is a more significant measure because heat of vaporization of the water formed in combustion cannot be recovered in aircraft exhaust. The most desirable gas turbine fuels for use in aircraft, after hydrogen, are hydrocarbons. Fuels that are liquid at normal atmospheric pressure and temperature are the most practical and widely used aircraft fuels kerosene, with a distillation range from 150 to 300 °C, is the best compromise to combine maximum mass —heat content with other desirable properties. For ground turbines, a wide variety of gaseous and heavy fuels are acceptable. [Pg.412]

Reasonably low pressures for operating temperatures Low specific heat of liquid High specific heat of vapor... [Pg.1124]

Liquid injection. Add volatile liquid so that the latent heat of vaporization equals excess energy. [Pg.1568]

A common cause of a BLE T] in plants of the hydrocarbon-chemical industry is exposure to fire. With an external fire below the liquid level in a vessel, the heat of vaporization provides a heat sink, as with a teakettle evolved vapors exit tnrough the relief valve. But if the flame impinges on the vessel above the liquid level, the metal will weaken and may cause the vessel to rupture suddenly, even with the relief valve open. The explosive energy for a BLE T] comes from superheat. This energy is at a maximum at the superheat hmit temperature. (SLT is the maximum temperature to which a hquid can be heated before homogeneous nucleation occurs with explosive vaporization of the hquid and accompanying overpressure.) The SLT... [Pg.2321]

The resulting data for liquid metals indicate a systematic relationship witlr the bonding energy of the element, which is reflected in the heat of vaporization... [Pg.295]

In addition to volume changes the effect of temperature is also important. Thus the specific latent heat of vaporization of a chemical is the quantity of heat, expressed as kJ/kg, required to change unit mass of liquid to vapour with no associated change in temperature. This heat is absorbed on vaporization so tliat residual liquid or tlie sunoundings cool. Alternatively an equivalent amount of heat must be removed to bring about condensation. Thus the temperature above a liquefied gas is reduced as tlie liquid evaporates and tlie bulk liquid cools. There may be consequences for heat transfer media and the strength of construction materials at low temperatures. [Pg.47]

Latent Heat of Vaporization The heat required to change a liquid into a vapor without a change in the temperature or pressure. [Pg.91]


See other pages where Heat of vaporization, liquids is mentioned: [Pg.303]    [Pg.56]    [Pg.499]    [Pg.349]    [Pg.499]    [Pg.175]    [Pg.346]    [Pg.754]    [Pg.465]    [Pg.303]    [Pg.56]    [Pg.499]    [Pg.349]    [Pg.499]    [Pg.175]    [Pg.346]    [Pg.754]    [Pg.465]    [Pg.236]    [Pg.74]    [Pg.513]    [Pg.502]    [Pg.476]    [Pg.294]    [Pg.471]    [Pg.1359]    [Pg.1360]    [Pg.2291]    [Pg.2292]    [Pg.292]    [Pg.20]    [Pg.17]    [Pg.83]    [Pg.65]    [Pg.117]    [Pg.175]    [Pg.1]    [Pg.1]   
See also in sourсe #XX -- [ Pg.59 , Pg.60 , Pg.159 ]




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