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Conduction equation specific

One of the most important parts of the fuel cell is the electrolyte. For polymer-electrolyte fuel cells this electrolyte is a single-ion-conducting membrane. Specifically, it is a proton-conducting membrane. Although various membranes have been examined experimentally, most models focus on Nafion. Furthermore. it is usually necessary only to modify property values and not governing equations if one desires to model other membranes. The models presented and the discussion below focus on Nafion. [Pg.451]

Surfactant Activity in Micellar Systems. The activities or concentrations of individual surfactant monomers in equilibrium with mixed micelles are the most important quantities predicted by micellar thermodynamic models. These variables often dictate practical performance of surfactant solutions. The monomer concentrations in mixed micellar systems have been measured by ultraf i Itration (I.), dialysis (2), a combination of conductivity and specific ion electrode measurements (3), a method using surface tension of mixtures at and above the CMC <4), gel filtration (5), conductivity (6), specific ion electrode measurements (7), NMR <8), chromatograph c separation of surfactants with a hydrophilic substrate (9> and by application of the Bibbs-Duhem equation to CMC data (iO). Surfactant specific electrodes have been used to measure anionic surfactant activities in single surfactant systems (11.12) and might be useful in mixed systems. ... [Pg.325]

AirCIri). This is an executable program for any air-cooler condenser. The inputted Q will be the heat duty transferred. Data inputs for condenser tube-side transport property values of viscosity, thermal conductivity, and specific heat should be determined as for two-phase flow values calculated in Chap. 6. Use the average tube-side temperature for these condensing film transport property values. Weighted average values between gas and liquid should also be determined and applied like that used in the two-phase flow equations in Chap. 6. [Pg.208]

Under these conditions, the variation of the temperature profile (during irradiation with constant flux) could be computed from the heat-conduction equation in terms of the thermal conductivity, k the absorbance, a the incident flux, H the specific heat capacity, c and the thermal diffusivity, a. With the boundary conditions ... [Pg.450]

Now consider a sphere, with density p, specific heat c, and outer radius R. The area of the sphere normal to the direclion of heat transfer at any location is A — 4vrr where r is the value of the radius at that location. Note that the heat transfer area A depends on r in this case also, and thus it varies with location. By considering a thin spherical shell element of thickness Ar and repeating tile approach described above for the cylinder by using A = 4 rrr instead of A = InrrL, the one-dimensional transient heat conduction equation for a sphere is determined to be (Fig. 2-17)... [Pg.91]

In the derivation of the heat conduction equation in (2.8) we presumed an incompressible body, g = const. The temperature dependence of both the thermal conductivity A and the specific heat capacity c was also neglected. These assumptions have to be made if a mathematical solution to the heat conduction equation is to be obtained. This type of closed solution is commonly known as the exact solution. The solution possibilities for a material which has temperature dependent properties will be discussed in section 2.1.4. [Pg.109]

In combination with specific conductance (equation 7) and modified Ohm s law (equation 6), it follows that... [Pg.202]

Equation (11.1) is essentially a solution of Eq. (11.7) and is based on a few assumptions and simplifications, e.g., no axial heat conduction, constant average heat conductivity and specific heat, constant heat source, steady-state heat transfer, one-dimensional (radial) heat flux, cylindrical geometry in the waste and in the surrounding material, e.g., salt, and no heat source in the salt. [Pg.583]

As described in the previous sections, the changes in the effective thermophysical properties (density, thermal conductivity, and specific heat capacity) are mainly determined by the decomposition process. This process, being kinetic, is not just an univariate function of temperature, but also on time. Therefore, and in contrast to true material properties, effective properties are dependent not only on temperature, but also on time. In order to model the time-dependent physical properties, related kinetic processes must be taken into account, as described by the kinetic equations in Chapter 2. [Pg.70]

Models for the effective thermophysical properties - including mass (density), thermal conductivity, and specific heat capacity - have been developed in Chapter 4. Those material property models are implemented into the heat transfer governing equation in the following. [Pg.111]

Given the importance of low-Re, viscous flow on microscale aerodynamics, it is possible to take advantage of the dominant heat transfer effects to enhance microrotorcraft flight. These heat effects can be characterized using the standard transport equations and a Navier-Stokes solver. In order to accurately apply the physical properties, it is important to include the effect of temperature on the viscosity (using, e.g., Sutherland s, Wilke s, or Keyes laws), thermal conductivity, and specific heat of the surrounding fluid (air). [Pg.2146]

Equation (6.30) states that physical properties of tube side stream (namely, conductivity k, specific heat capacity Cp), and mass velocity u have a positive effect on tube side film coefficient hi. In contrast, viscosity /u and tube inside diameter di have a negative effect. [Pg.91]

Models Based on a Desorption-Dissolution-Diffusion Mechanism in a Porous Sphere. The precursor of these models was the application by Bartle et. al [20] of the Pick s law of diflusion (or the heat conduction equation, i.e. the Fourier equation) to SFE of spherical particles. In doing so they had to assume an initial uniform distribution of the material extracted (in this specific case 1-8 cineole) from rosemary particles. Since Pick s law of difiusion from a sphere is analogous to a cooling hot ball (Crank [21] vs Carslaw and Jaeger [22]), this type of models have been considered to be analogous to heat transfer. This model was also used by Reverchon and his co-workers [23] and [24] to SFE of basil, rosemary and marjoram with some degree of success. [Pg.505]

In each equation the dependent variable, T, is a function of four independent variables, x, y, z, t) (r, cp, z, t) (r, q), 0, f) and is a second-order, partial differential equation. In order to solve the differential conduction equation for specific problem, two boundary conditions and one initial condition are required. [Pg.732]

Conservation equations include physical quantities, such as density, viscosity, thermal conductivity, or specific heat. These quantities do not depend on conservation equations but are unique to a specific fluid or material that needs to be used to represent a real-world physical system. Therefore, a CFD engineer has to choose appropriate physical properties from experimental data, literature, databases, or built-in libraries embedded in CFD and multiphysics software tools. Only properly assigned physical properties will adequately describe conservation equations. [Pg.222]

Here L is the sample length, d is the diameter, m is the mass, Cp is the specimen s specific-heat capacity, C is the measured apparent heat capacity of the thick sample, and P is the modulation period. Derivation of the thermal conductivity equations for MTDSC can be found in Blaine and Marcus... [Pg.204]

From Equation 4.6, we can also see that the separator resistance is proportional to the thickness d and has a dependency on temperature and concentration of the electrolyte, which will impact the conductivity. The specific conductivity of sulfuric acid in typical batteries with a density of 1.28 g/cm- at 25°C is 1.26 Q. cm. [Pg.117]

Here, K and Cp are, respectively, the thermal conductivity and specific heat capacity of the fluid. The viscous dissipation

strain rate tensor, e = i(V + (Vm) ). The second term of equation (7.59) is the ohmic heating due to the passage of the current. [Pg.297]


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See also in sourсe #XX -- [ Pg.7 , Pg.8 ]




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