PROBLEMS

5.2-1.

Temperature Response in Cooling a Wire. A small copper wire with a diameter of 0.792 mm and initially at 366.5 K is suddenly immersed in a liquid held constant at 311 K. The convection coefficient h = 85.2 W/m2 · K. The physical properties can be assumed constant and are k = 374 W/m · K, cp = 0.389 kJ/kg · K, and ρ = 8890 kg/m3.

  1. Determine the time in seconds for the average temperature of the wire to drop to 338.8 K (one-half the initial temperature difference).

  2. Do the same but for h = 11.36 W/m2 · K.

  3. For part (b), calculate the total amount of heat removed for a wire 1.0 m long.

A1: Ans. (a) t = 5.66 s
5.2-2.

Quenching Lead Shot in a Bath. Lead shot having an average diameter of 5.1 mm is at an initial temperature of 204.4°C. To quench the shot it is added to a quenching oil bath held at 32.2°C and falls to the bottom. The time of fall is 15 s. Assuming an average convection coefficient of h = 199 W/m2 · K, what will be the temperature of the shot after the fall? For lead, ρ = 11 370 kg/m3 and cp = 0.138 kJ/kg · K.

5.2-3.

Unsteady-State Heating of a Stirred Tank. A vessel is filled with 0.0283 m3 of water initially at 288.8 K. The vessel, which is well stirred, is suddenly immersed in a steam bath held at 377.6 K. The overall heat-transfer coefficient U between the steam and water is 1136 W/m2 · K and the area is 0.372 m2. Neglecting the heat capacity of the walls and agitator, calculate the time in hours to heat the water to 338.7 K. [Hint: Since the water is well stirred, its temperature is uniform. Show that Eq. (5.2-3) holds by starting with Eq. (5.2-1).]

5.3-1.

Temperature in a Refractory Lining. A combustion chamber has a 2-in.-thick refractory lining to protect the outer shell. To predict the thermal stresses at start-up, the temperature 0.2 in. below the surface is needed 1 min after start-up. The following data are available. The initial temperature T0 = 100°F, the hot gas temperature T1 = 3000°F, h = 40 btu/h · ft2 · °F, k = 0.6 btu/h · ft · °F, and α = 0.020 ft2/h. Calculate the temperature at a 0.2-in. depth and a 0.6-in. depth. Use Fig. 5.3-3 and justify its use by seeing if the lining acts as a semi-infinite solid during this 1-min period.

A4: Ans. For x = 0.2 in., (TT0)/(T1T0) = 0.28 and T = 912°F (489°C); for x = 0.6 in., (TT0)/(T1T0) = 0.02 and T = 158°F (70°C)
5.3-2.

Freezing Temperature in the Soil. The average temperature of the soil to a considerable depth is approximately 277.6 K (40°F) during a winter day. If the outside air temperature suddenly drops to 255.4 K (0°F) and stays there, how long will it take for a pipe 3.05 m (10 ft) below the surface to reach 273.2 K (32°F)? The convective coefficient is h = 8.52 W/m2 · K (1.5 btu/h · ft2 · °F). The soil physical properties can be taken as 5.16 × 107 m2/s (0.02 ft2/h) for the thermal diffusivity and 1.384 W/m · K (0.8 btu/h · ft · °F) for the thermal conductivity. (Note: The solution is trial and error, since the unknown time appears twice in the graph for a semi-infinite solid.)

5.3-3.

Cooling a Slab of Aluminum. A large piece of aluminum that can be considered a semi-infinite solid initially has a uniform temperature of 505.4 K. The surface is suddenly exposed to an environment at 338.8 K with a surface convection coefficient of 455 W/m2 · K. Calculate the time in hours for the temperature to reach 388.8 K at a depth of 25.4 mm. The average physical properties are α = 0.340 m2/h and k = 208 W/m · K.

5.3-4.

Transient Heating of a Concrete Wall. A wall made of concrete 0.305 m thick is insulated on the rear side. The wall at a uniform temperature of 10°C (283.2 K) is exposed on the front side to a gas at 843°C (1116.2 K). The convection coefficient is 28.4 W/m2 · K, the thermal diffusivity is 1.74 × 103 m2/h, and the thermal conductivity is 0.935 W/m · K.

  1. Calculate the time for the temperature at the insulated face to reach 232°C (505.2 K).

  2. Calculate the temperature at a point 0.152 m below the surface at this same time.

A7: Ans. (a) ,t =13.4 h
5.3-5.

Cooking a Slab of Meat. A slab of meat 25.4 mm thick originally at a uniform temperature of 10°C is to be cooked from both sides until the center reaches 121°C in an oven at 177°C. The convection coefficient can be assumed constant at 25.6 W/m2 · K. Neglect any latent heat changes and calculate the time required. The thermal conductivity is 0.69 W/m · K and the thermal diffusivity 5.85 × 104 m2/h. Use the Heisler chart.

A8: Ans. 0.80 h (2880 s)
5.3-6.

Unsteady-State Conduction in a Brick Wall. A flat brick wall 1.0 ft thick is the lining on one side of a furnace. If the wall is at a uniform temperature of 100°F and one side is suddenly exposed to a gas at 1100°F, calculate the time for the furnace wall at a point 0.5 ft from the surface to reach 500°F. The rear side of the wall is insulated. The convection coefficient is 2.6 btu/h · ft2 · °F and the physical properties of the brick are k = 0.65 btu/h · ft · °F and α = 0.02 ft2/h.

5.3-7.

Cooling a Steel Rod. A long steel rod 0.305 m in diameter is initially at a temperature of 588 K. It is immersed in an oil bath maintained at 311 K. The surface convective coefficient is 125 W/m2 · K. Calculate the temperature at the center of the rod after 1 h. The average physical properties of the steel are k = 38 W/m · K and α = 0.0381 m2/h.

A10: Ans. T = 391 K
5.3-8.

Effect of Size on Heat Processing Meat. An autoclave held at 121.1°C is being used to process sausage meat 101.6 mm in diameter and 0.61 m long which is originally at 21.1°C. After 2 h the temperature at the center is 98.9°C. If the diameter is increased to 139.7 mm, how long will it take for the center to reach 98.9°C? The heat-transfer coefficient to the surface is h = 1100 W/m2 · K, which is very large, so the surface resistance can be considered negligible. (Show this.) Neglect the heat transfer from the ends of the cylinder. The thermal conductivity k = 0.485 W/m · K.

A11: Ans. 3.78 h
5.3-9.

Temperature of Oranges on Trees During Freezing Weather. In orange-growing areas, the freezing of the oranges on the trees during cold nights is of serious economic concern. If the oranges are initially at a temperature of 21.1°C, calculate the center temperature of the orange if exposed to air at −3.9°C for 6 h. The oranges are 102 mm in diameter and the convective coefficient is estimated as 11.4 W/m2 · K. The thermal conductivity k is 0.431 W/m · K and α is 4.65 × 104 m2/h. Neglect any latent heat effects.

A12: Ans. (T1T)/(T1T0) = 0.05, T = −2.65°C
5.3-10.

Hardening a Steel Sphere. To harden a steel sphere having a diameter of 50.8 mm, it is heated to 1033 K and then dunked into a large water bath at 300 K. Determine the time for the center of the sphere to reach 366.5 K. The surface coefficient can be assumed as 710 W/m2 · K, k = 45 W/m · K, and α = 0.0325 m2/h.

5.3-11.

Unsteady-State Conduction in a Short Cylinder. An aluminum cylinder is initially heated to a uniform temperature of 204.4°C. Then it is plunged into a large bath held at 93.3°C, where h = 568 W/m2 · K. The cylinder has a diameter of 50.8 mm and is 101.6 mm long. Calculate the center temperature after 60 s. The physical properties are α = 9.44 × 105 m2/s and k = 207.7 W/m · K.

5.3-12.

Conduction in Three Dimensions in a Rectangular Block. A rectangular steel block 0.305 m by 0.457 m by 0.61 m is initially at 315.6°C. It is suddenly immersed in an environment at 93.3°C. Determine the temperature at the center of the block after 1 h. The surface convection coefficient is 34 W/m2 · K. The physical properties are k = 38 W/m · K and α = 0.0379 m2/h.

5.4-1.

Schmidt Numerical Method for Unsteady-State Conduction. A material in the form of an infinite plate 0.762 m thick is at an initial uniform temperature of 366.53 K. The rear face of the plate is insulated. The front face is suddenly exposed to a temperature of 533.2 K. The convective resistance at this face can be assumed as zero. Calculate the temperature profile after 0.875 h using the Schmidt numerical method with M = 2 and slabs 0.1524 m thick. The thermal diffusivity is 0.0929 m2/h.

A16: Ans. Δt = 0.125 h, seven time increments needed
5.4-2.

Unsteady-State Conduction with Nonuniform Initial Temperature Profile. Use the same conditions as in Problem 5.4-1 but with the following change. The initial temperature profile is not uniform but is 366.53 K at the front face and 422.1 K at the rear face with a linear variation between the two faces.

5.4-3.

Unsteady-State Conduction Using the Digital Computer. Repeat Problem 5.4-2 but use the computer and a spreadsheet. Use slabs 0.03048 m thick and M = 2.0. Calculate the temperature profile after 0.875 h.

5.4-4.

Chilling Meat Using Numerical Methods. A slab of beef 45.7 mm thick and initially at a uniform temperature of 283 K is being chilled by a surface contact cooler at 274.7 K on the front face. The rear face of the meat is insulated. Assume that the convection resistance at the front surface is zero. Using five slices and M = 2, calculate the temperature profile after 0.54 h. The thermal diffusivity is 4.64 × 104 m2/h.

A19: Ans. Δt = 0.090 h, six time increments
5.4-5.

Cooling Beef with Convective Resistance. A large slab of beef is 45.7 mm thick and is at an initial uniform temperature of 37.78°C. It is being chilled at the front surface in a chilled air blast at −1.11°C with a convective heat-transfer coefficient of h = 38.0 W/m2 · K. The rear face of the meat is insulated. The thermal conductivity of the beef is k = 0.498 W/m · K and α = 4.64 × 104 m2/h. Using a numerical method with five slices and M = 4.0, calculate the temperature profile after 0.27 h. [Hint: Since there is a convective resistance, the value of N must be calculated. Also, Eq. (5.4-7) should be used.]

A20: Ans. 17.16°C (n = 1), 28.22°C (2), 34.48°C (3), 37.00°C (4), 37.67°C (5), 37.77°C (6)
5.4-6.

Cooling Beef Using the Digital Computer. Repeat Problem 5.4-5 using the digital computer. Use 20 slices and M = 4.0. Use a spreadsheet calculation.

5.4-7.

Convection and Unsteady-State Conduction. For the conditions of Example 5.4-3, continue the calculations for a total of 12 time increments. Plot the temperature profile.

5.4-8.

Alternative Convective Boundary Condition for Numerical Method. Repeat Example 5.4-3 but instead use the alternative boundary condition, Eq. (5.4-11). Also, use M = 4. Calculate the profile for the full 12 time increments.

5.4-9.

Numerical Method for Semi-infinite Solid and Convection. A semi-infinite solid initially at a uniform temperature of 200°C is cooled at its surface by convection. The cooling fluid at a constant temperature of 100°C has a convective coefficient of h = 250 W/m2 · K. The physical properties of the solid are k = 20 W/m · K and α = 4 × 105 m2/s. Using a numerical method with Δx = 0.040 m and M = 4.0, calculate the temperature profile after 50 s total time.

A24: Ans. T1 = 157.72, T2 = 181.84, T3 = 194.44, T4 = 198.93, T5 = 199.90°C
5.5-1.

Chilling Slab of Beef. Repeat Example 5.5-1, where the slab of beef is cooled to 10°C at the center, but use air of 0°C at a lower value of h = 22.7 W/m2 · K.

A25: Ans. (T1T)/(T1T0) = 0.265, X = 0.92, t = 19.74 h
5.5-2.

Chilling Fish Fillets. Codfish fillets originally at 10°C are packed to a thickness of 102 mm. Ice is packed on both sides of the fillets and wet-strength paper separates the ice and fillets. The surface temperature of the fish can be assumed as essentially 0°C. Calculate the time for the center of the fillets to reach 2.22°C and the temperature at this time at a distance of 25.4 mm from the surface. Also, plot temperature versus position for the slab. The physical properties are (B1) k = 0.571 W/m · K, ρ = 1052 kg/m3, and cp = 4.02 kJ/kg · K.

5.5-3.

Average Temperature in Chilling Fish. Fish fillets having the same physical properties given in Problem 5.5-2 are originally at 10°C. They are packed to a thickness of 102 mm with ice on each side. Assuming that the surface temperature of the fillets is 0°C, calculate the time for the average temperature to reach 1.39°C. (Note: This is a case where the surface resistance is zero. Can Fig. 5.3-13 be used for this case?)

5.5-4.

Time to Freeze a Slab of Meat. Repeat Example 5.5-2 using the same conditions except that a plate or contact freezer is used where the surface coefficient can be assumed as h = 142 W/m2 · K.

A28: Ans. t = 2.00 h
5.5-5.

Freezing a Cylinder of Meat. A package of meat containing 75% moisture and in the form of a long cylinder 5 in. in diameter is to be frozen in an air-blast freezer at −25°F. The meat is initially at the freezing temperature of 27°F. The heat-transfer coefficient is h = 3.5 btu/h · ft2 · °F. The physical properties are ρ = 64 lbm/ft3 for the unfrozen meat and k = 0.60 btu/h · ft · °F for the frozen meat. Calculate the freezing time.

5.6-1.

Heat Generation Using Equation of Energy Change. A plane wall with uniform internal heat generation of W/m3 is insulated at four surfaces, with heat conduction only in the x direction. The wall has a thickness of 2L m. The temperature at one wall at x = +L and at the other wall at x = −L is held constant at Tw K. Using the differential equation of energy change, Eq. (5.6-18), derive the equation for the final temperature profile.

A30: Ans.
5.6-2.

Heat Transfer in a Solid Using Equation of Energy Change. A solid of thickness L is at a uniform temperature of T0 K. Suddenly the front surface temperature of the solid at z = 0 m is raised to T1 at t = 0 and held there, and at z = L at the rear to T2 and held constant. Heat transfer occurs only in the z direction. For constant physical properties and using the differential equation of energy change, do as follows:

  1. Derive the partial differential equation and the boundary conditions (B.C.) for unsteady-state energy transfer.

  2. Do the same for steady state and integrate the final equation.

A31: Ans. (a) ∂T/∂t = α ∂2T/∂z2; B.C.(1): t = 0, z = z, T = T0; B.C.(2): t = t, z = 0, T = T1; B.C.(3): t = t, z = L, T = T2; (b) T = (T2T1)z/L + T1
5.6-3.

Radial Temperature Profile Using the Equation of Energy Change. Radial heat transfer is occurring by conduction through a long, hollow cylinder of length L with the ends insulated.

  1. What is the final differential equation for steady-state conduction? Start with Fourier's second law in cylindrical coordinates, Eq. (5.6-20).

  2. Solve the equation for the temperature profile from part (a) for the boundary conditions given as follows: T = Ti for r = ri, T = To for r = ro.

  3. Using part (b), derive an expression for the heat flow q in W.

A32: Ans.
5.6-4.

Heat Conduction in a Sphere. Radial energy flow is occurring in a hollow sphere with an inside radius of ri and an outside radius of ro. At steady state the inside surface temperature is constant at Ti and constant at To on the outside surface.

  1. Using the differential equation of energy change, solve the equation for the temperature profile.

  2. Using part (a), derive an expression for the heat flow in W.

5.6-5.

Variable Heat Generation and Equation of Energy Change. A plane wall is insulated so that conduction occurs only in the x direction. The boundary conditions which apply at steady state are T = T0 at x = 0 and T = TL at x = L. Internal heat generation per unit volume is occurring and varies as , where and ß are constants. Solve the general differential equation of energy change for the temperature profile.

5.7-1.

Thermal and Hydrodynamic Boundary Layer Thicknesses. Air at 294.3 K and 101.3 kPa with a free stream velocity of 12.2 m/s is flowing parallel to a smooth, flat plate held at a surface temperature of 383 K. Do the following:

  1. At the critical NRe,L = 5 × 105, calculate the critical length x = L of the plate, the thickness δ of the hydrodynamic boundary layer, and the thickness δT of the thermal boundary layer. Note that the Prandtl number is not 1.0.

  2. Calculate the average heat-transfer coefficient over the plate covered by the laminar boundary layer.

5.7-2.

Boundary-Layer Thicknesses and Heat Transfer. Air at 37.8°C and 1 atm abs flows at a velocity of 3.05 m/s parallel to a flat plate held at 93.3°C. The plate is 1 m wide. Calculate the following at a position 0.61 m from the leading edge:

  1. The thermal boundary-layer thickness δT and the hydrodynamic boundary-layer thickness δ.

  2. Total heat transfer from the plate.

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