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Nonisothermal Piston Flow

FIGURE 5.3 Differential element in a nonisothermal piston flow reactor. [Pg.164]

Unlike a molar flow rate—e.g, aQ—the mass flow rate, pQ, is constant and can be brought outside the differential. Note that Q = uAc and that is the external surface area per unit length of tube. Equation (5.22) can be written as [Pg.164]

This equation is coupled to the component balances in Equation (3.9) and with an equation for the pressure e.g., one of Equations (3.14), (3.15), (3.17). There are A +2 equations and some auxiliary algebraic equations to be solved simultaneously. Numerical solution techniques are similar to those used in Section 3.1 for variable-density PFRs. The dependent variables are the component fluxes I , the enthalpy H, and the pressure P. A necessary auxiliary equation is the thermodynamic relationship that gives enthalpy as a function of temperature, pressure, and composition. Equation (5.16) with Tref=0 is the simplest example of this relationship and is usually adequate for preliminary calculations. [Pg.164]

With a constant, circular cross section, A = 2jiR (although the concept of piston flow is not restricted to circular tubes). If Cp is constant, [Pg.164]

This is the form of the energy balance that is usually used for preliminary calculations. Equation (5.24) does not require that u be constant. If it is constant, we can set dz = udt and 2IR = AextlAc to make Equation (5.24) identical to Equation (5.19). A constant-velocity, constant-properties PER behaves [Pg.164]

Steady state and differential quantities are now used. The pQH terms cancel and Az factors out to give [Pg.176]

This equation is coupled to the component balances of Equation 3.9 and with an equation for the pressure, for example, one of Equations 3.18, 3.19, or 3.21. There are iV + 2 equations and some auxiliary algebraic equations that need to be solved simultaneously. Numerical solution techniques are similar to those used in Section [Pg.176]

1 for variable-density PFRs. The dependent variables are the component fluxes the enthalpy H, and the pressure P. A necessary auxiliary equation is the thermodynamic relationship that gives enthalpy as a function of temperature, pressure, and composition. Equation 5.15 with = 0 is the simplest example of this relationship and is usually adequate for preliminary calculations. [Pg.176]


Most kinetic experiments are run in batch reactors for the simple reason that they are the easiest reactor to operate on a small, laboratory scale. Piston flow reactors are essentially equivalent and are implicitly included in the present treatment. This treatment is confined to constant-density, isothermal reactions, with nonisothermal and other more complicated cases being treated in Section 7.1.4. The batch equation for component A is... [Pg.218]

Correlations for E are not widely available. The more accurate model given in Section 9.1 is preferred for nonisothermal reactions in packed-beds. However, as discussed previously, this model degenerates to piston flow for an adiabatic reaction. The nonisothermal axial dispersion model is a conservative design methodology available for adiabatic reactions in packed beds and for nonisothermal reactions in turbulent pipeline flows. The fact that E >D provides some basis for estimating E. Recognize that the axial dispersion model is a correction to what would otherwise be treated as piston flow. Thus, even setting E=D should improve the accuracy of the predictions. [Pg.337]

Example 9.6 Compare the nonisothermal axial dispersion model with piston flow for a first-order reaction in turbulent pipeline flow with Re= 10,000. Pick the reaction parameters so that the reactor is at or near a region of thermal runaway. [Pg.339]


See other pages where Nonisothermal Piston Flow is mentioned: [Pg.163]    [Pg.163]    [Pg.175]    [Pg.163]    [Pg.163]    [Pg.163]    [Pg.175]    [Pg.163]    [Pg.263]    [Pg.270]    [Pg.539]    [Pg.263]    [Pg.270]    [Pg.329]    [Pg.539]    [Pg.89]    [Pg.337]    [Pg.344]    [Pg.263]    [Pg.270]    [Pg.329]    [Pg.539]    [Pg.94]    [Pg.425]   


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