Thermal Energy Storage Systems and Applications. Ibrahim Dincer

Thermal Energy Storage Systems and Applications - Ibrahim  Dincer


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Eq. (1.86) is equal to Eq. (1.87), and hence to Eq. (1.90):

      (1.91)equation

      which yields

      (1.93)equation

      where, 1/H = (1/hA + L/k + 1/hB). H is the overall heat transfer coefficient and includes various heat transfer coefficients.

      1.6.3 Radiation Heat Transfer

      An object emits radiant energy in all directions unless its temperature is absolute zero. If this energy strikes a receiver, part of it may be absorbed, part may be transmitted, and part may be reflected. Heat transfer from a hot to a cold object in this manner is known as radiation heat transfer. The higher the temperature, the greater is the amount of energy radiated. If, therefore, two objects at different temperatures are placed so that the radiation from each object is intercepted by the other, then the body at the lower temperature will receive more energy than it radiates, and thereby its internal energy will increase; in conjunction with this, the internal energy of the object at the higher temperature will decrease. Radiation heat transfer frequently occurs between solid surfaces, although radiation from gases also takes place. Certain gases emit and absorb radiation at certain wavelengths only, whereas most solids radiate over a wide range of wavelengths. The radiative properties of many gases and solids may be found in heat transfer books.

      Radiation striking an object can be absorbed by the object, reflected from the object, or transmitted through the object. The fractions of the radiation absorbed, reflected, and transmitted are called the absorptivity a, the reflectivity r, and the transmissivity t, respectively. By definition, a + r + t = 1. For many solids and liquids in practical applications, the transmitted radiation is negligible, and hence a + r = 1. A body that absorbs all radiation striking it is called a blackbody. For a blackbody, a = 1 and r = 0.

      (c) The Stefan–Boltzmann Law

      (1.94)equation

      where, σ denotes the Stefan–Boltzmann constant, which has a value of 5.669 × 10−8 W/m2 K4, and Ts denotes the absolute temperature of the surface.

      The energy emitted by a non‐blackbody becomes

      (1.95)equation

      Then, the heat transferred from an object's surface to its surroundings per unit area is

      (1.96)equation

      Note that if the emissivity of the object at Ts is much different from the emissivity of the object at Ta, then this gray object approximation may not be sufficiently accurate. In this case, it is a good approximation to take the absorptivity of object 1 when receiving radiation from a source at Ta as being equal to the emissivity of object 1 when emitting radiation at Ta. This results in

      There are numerous applications for which it is convenient to express the net radiation heat transfer (radiation heat exchange) in the following form:

      (1.99)equation

      Here, the radiation heat transfer coefficient is seen to strongly depend on temperature, whereas the temperature dependence of the convection heat transfer coefficient is generally weak.

      The surface within the surroundings may also simultaneously transfer heat by convection to the surroundings. The total rate of heat transfer from the surface is the sum of the convection and radiation modes:

      (1.100)equation

      1.6.4 Thermal Resistance

      (1.101)equation

      (1.102)equation

      It is also possible to write the thermal resistance for convection, based on Eq. (1.85), as follows:

      (1.103)equation

      In a series of connected objects through which heat is transferred, the total thermal resistance can be written in terms of the overall heat transfer coefficient. The heat transfer expression for a composite wall is discussed next.

      1.6.5 The Composite Wall


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