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Heat flux potential

Internal Regenerator Bed Colls. Internal cods generate high overall heat-transfer coefficients [550 W / (m -K)] and typically produce saturated steam up to 4.6 MPa (667 psi). Lower heat fluxes are attained when producing superheated steam. The tube banks are normally arranged horizontally in rows of three or four, but because of their location in a continuously active bubbling or turbulent bed, they offer limited duty flexibdity with no shutdown or start-up potential. [Pg.219]

The water supply for boilers is usually treated. Treatment depends on the quality of the water supply, the pressure of the boiler, the heat flux through the tube walls and the steam quality required. Most waters require de-alkalization. The water produced in this process is nonscaling and potentially corrosive (see above). [Pg.898]

In summary, it follows that temperature may be viewed as a potential for heat flux, pressure as a potential for volume change and p as a chemical potential for matter flow. [Pg.416]

Design practices stem from standard fire test procedures in which the temperature history of the test furnace is regarded as an index of the destructive potential of a fire. Thus, the practice of describing the expected effects and damage mechanism is based on temperature histories. This standard design practice is convenient but lacks accuracy in terms of structural performance. The severity of a fire should address the expected intensity of the heat flux that will impact the structure and the duration of heat penetration. A simple analysis of the expect nature of an unwanted fire can be based on the heats of combustion and pyrolysis of the principal contents in the facility. The heat of combustion will identify the destructive nature of the fire, while the heat of pyrolysis will identify the severity of the fire within the compartment itself and will also identify the destructive potential of the fire in adjacent spaces. [Pg.149]

Velocity and temperature gradients are confined to the surface layer defined by z < I-. Above L the wind velocity and potential temperature are virtually uniform with height. Venkatram (1978) has presented a method to estimate the value of the convective velocity scale w,. On the basis of this method, he showed that convective conditions in the planetary boundary layer are a common occurrence (Venkatram, 1980). In particular, the planetary boundary layer is convective during the daytime hours for a substantial fraction of each year ( 7 months). For example, for a wind speed of 5 m sec , a kinematic heat flux Qo as small as O.PC sec can drive the planetary boundary layer into a convective state. [Pg.261]

However, some of these mine waters have significant potential for energy recovery via use of heat pumps. For example, the Morlais mine water of South Wales has an estimated discharge of at least 100 L/s. The specific heat capacity of water is around 4181 J/L/°C or 1.16kWh/m3/ °C. If the Morlais mine water s temperature could be lowered by using a heat pump by 5 °C (from 14 to 9 °C), a heat flux (power) of ... [Pg.505]

The thermoelectric effect is due to the gradient in electrochemical potential caused by a temperature gradient in a conducting material. The Seebeck coefficient a is the constant of proportionality between the voltage and the temperature gradient which causes it when there is no current flow, and is defined as (A F/A7) as AT- 0 where A Fis the thermo-emf caused by the temperature gradient AT it is related to the entropy transported per charge carrier (a = — S /e). The Peltier coefficient n is the proportionality constant between the heat flux transported by electrons and the current density a and n are related as a = Tr/T. [Pg.304]

There are two types of differential scanning calorimeters (a) heat flux (AT) and (b) power compensation (AT). Subsequent sections of this experiment will not distinguish between the two types. In either type of calorimeter, the measurement is compared to that for a reference material having a known specific heat [16,17], As AT and AT have opposite signs there is some potential for confusion [3], e.g., at the melting point, Tm, Ts < Tr, and AT < 0, whereas Ts > Tr and AT > 0 because latent heat must be supplied (subscripts s and r refer to the sample and the reference material, respectively) [3]. [Pg.120]

In addition to simply solving the differential equation, we seek to use the solution to understand and quantify the heat transfer between the fluid and the duct walls. The heat flux q" (W/m2) can be described in terms of a heat-transfer coefficient h (W/m2 K), with the thermal driving potential being the difference between the wall temperature and the mean fluid temperature ... [Pg.189]

By tuning the potential difference, the device can emit a certain radiation spectrum by varying the incident radiation, the device can generate various electrical currents. In this instance, it is important to concentrate on the electron flux N, just as we did on the heat flux Q in photothermal energy... [Pg.313]

Once the electric potential is impressed on the paper, an ordinary voltmeter may be used to plot lines of constant electric potential. With these constant-potential lines available, the flux lines may be easily constructed since they are orthogonal to the potential lines. These equipotential and flux lines have precisely the same arrangement as the isotherms and heat-flux lines in the corresponding heat-conduction problem. The shape factor is calculated immediately using the method which was applied to the curvilinear squares. [Pg.117]

Consider the reason for the appearance of the thermomechanical effect and its expected value. Let us say that two vessels, 1 and 2, are filled with some identical fluid (hquid or gas) and connected by a capillary, the fluids being held at preset constant temperatures T and T + dT. Let Jq desig nate the heat flux that passes through the capillary between the vessels, while Jg designates a potential fluid flux that diffuses through the same cap iUary (Figure 2.3). In accordance to the preceding deduced relationships (also see Section 1.5), the thermodynamic forces that initiate the fluxes are determined by the formula... [Pg.80]


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See also in sourсe #XX -- [ Pg.416 ]




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Heat Potentials

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