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Fundamentals of heat and mass transfer frank p incropera david p dewitt solution manual ch1 (1 40)

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Microsoft Word problem1 01 doc PROBLEM 1 1 KNOWN Heat rate, q, through one dimensional wall of area A, thickness L, thermal conductivity k and inner temperature, T1 FIND The outer temperature of the w[.]

PROBLEM 1.1 KNOWN: Heat rate, q, through one-dimensional wall of area A, thickness L, thermal conductivity k and inner temperature, T1 FIND: The outer temperature of the wall, T2 SCHEMATIC: ASSUMPTIONS: (1) One-dimensional conduction in the x-direction, (2) Steady-state conditions, (3) Constant properties ANALYSIS: The rate equation for conduction through the wall is given by Fourier’s law, q cond = q x = q ′′x ⋅ A = -k T −T dT ⋅ A = kA dx L Solving for T2 gives T2 = T1 − q cond L kA Substituting numerical values, find T2 = 415$ C - 3000W × 0.025m 0.2W / m ⋅ K × 10m2 T2 = 415$ C - 37.5$ C T2 = 378$ C COMMENTS: Note direction of heat flow and fact that T2 must be less than T1 < PROBLEM 1.2 KNOWN: Inner surface temperature and thermal conductivity of a concrete wall FIND: Heat loss by conduction through the wall as a function of ambient air temperatures ranging from -15 to 38°C SCHEMATIC: ASSUMPTIONS: (1) One-dimensional conduction in the x-direction, (2) Steady-state conditions, (3) Constant properties, (4) Outside wall temperature is that of the ambient air ANALYSIS: From Fourier’s law, it is evident that the gradient, dT dx = − q′′x k , is a constant, and hence the temperature distribution is linear, if q′′x and k are each constant The heat flux must be constant under one-dimensional, steady-state conditions; and k is approximately constant if it depends only weakly on temperature The heat flux and heat rate when the outside wall temperature is T2 = -15°C are ) ( 25$ C − −15$ C dT T1 − T2 q′′x = − k =k = 1W m ⋅ K = 133.3W m dx L 0.30 m q x = q′′x × A = 133.3 W m × 20 m = 2667 W (1) (2) < Combining Eqs (1) and (2), the heat rate qx can be determined for the range of ambient temperature, -15 ≤ T2 ≤ 38°C, with different wall thermal conductivities, k 3500 Heat loss, qx (W) 2500 1500 500 -500 -1500 -20 -10 10 20 30 40 Ambient air temperature, T2 (C) Wall thermal conductivity, k = 1.25 W/m.K k = W/m.K, concrete wall k = 0.75 W/m.K For the concrete wall, k = W/m⋅K, the heat loss varies linearily from +2667 W to -867 W and is zero when the inside and ambient temperatures are the same The magnitude of the heat rate increases with increasing thermal conductivity COMMENTS: Without steady-state conditions and constant k, the temperature distribution in a plane wall would not be linear PROBLEM 1.3 KNOWN: Dimensions, thermal conductivity and surface temperatures of a concrete slab Efficiency of gas furnace and cost of natural gas FIND: Daily cost of heat loss SCHEMATIC: ASSUMPTIONS: (1) Steady state, (2) One-dimensional conduction, (3) Constant properties ANALYSIS: The rate of heat loss by conduction through the slab is T −T 7°C q = k ( LW ) = 1.4 W / m ⋅ K (11m × m ) = 4312 W t 0.20 m < The daily cost of natural gas that must be combusted to compensate for the heat loss is Cd = q Cg ηf ( ∆t ) = 4312 W × $0.01/ MJ 0.9 ×106 J / MJ ( 24 h / d × 3600s / h ) = $4.14 / d < COMMENTS: The loss could be reduced by installing a floor covering with a layer of insulation between it and the concrete PROBLEM 1.4 KNOWN: Heat flux and surface temperatures associated with a wood slab of prescribed thickness FIND: Thermal conductivity, k, of the wood SCHEMATIC: ASSUMPTIONS: (1) One-dimensional conduction in the x-direction, (2) Steady-state conditions, (3) Constant properties ANALYSIS: Subject to the foregoing assumptions, the thermal conductivity may be determined from Fourier’s law, Eq 1.2 Rearranging, k=q′′x L W = 40 T1 − T2 m2 k = 0.10 W / m ⋅ K 0.05m ( 40-20 ) C < COMMENTS: Note that the °C or K temperature units may be used interchangeably when evaluating a temperature difference PROBLEM 1.5 KNOWN: Inner and outer surface temperatures of a glass window of prescribed dimensions FIND: Heat loss through window SCHEMATIC: ASSUMPTIONS: (1) One-dimensional conduction in the x-direction, (2) Steady-state conditions, (3) Constant properties ANALYSIS: Subject to the foregoing conditions the heat flux may be computed from Fourier’s law, Eq 1.2 T −T q′′x = k L  W (15-5 ) C q′′x = 1.4 m ⋅ K 0.005m q′′x = 2800 W/m Since the heat flux is uniform over the surface, the heat loss (rate) is q = q ′′x × A q = 2800 W / m2 × 3m2 q = 8400 W COMMENTS: A linear temperature distribution exists in the glass for the prescribed conditions < PROBLEM 1.6 KNOWN: Width, height, thickness and thermal conductivity of a single pane window and the air space of a double pane window Representative winter surface temperatures of single pane and air space FIND: Heat loss through single and double pane windows SCHEMATIC: ASSUMPTIONS: (1) One-dimensional conduction through glass or air, (2) Steady-state conditions, (3) Enclosed air of double pane window is stagnant (negligible buoyancy induced motion) ANALYSIS: From Fourier’s law, the heat losses are Single Pane: T1 − T2 35 $C qg = k g A = 1.4 W/m ⋅ K 2m = 19, 600 W L 0.005m ( ) ( ) T −T 25 $C Double Pane: qa = k a A = 0.024 2m2 = 120 W L 0.010 m COMMENTS: Losses associated with a single pane are unacceptable and would remain excessive, even if the thickness of the glass were doubled to match that of the air space The principal advantage of the double pane construction resides with the low thermal conductivity of air (~ 60 times smaller than that of glass) For a fixed ambient outside air temperature, use of the double pane construction would also increase the surface temperature of the glass exposed to the room (inside) air PROBLEM 1.7 KNOWN: Dimensions of freezer compartment Inner and outer surface temperatures FIND: Thickness of styrofoam insulation needed to maintain heat load below prescribed value SCHEMATIC: ASSUMPTIONS: (1) Perfectly insulated bottom, (2) One-dimensional conduction through walls of area A = 4m , (3) Steady-state conditions, (4) Constant properties ANALYSIS: Using Fourier’s law, Eq 1.2, the heat rate is q = q ′′ ⋅ A = k ∆T A total L Solving for L and recognizing that Atotal = 5×W , find k ∆ T W2 L = q  L= ( ) × 0.03 W/m ⋅ K 35 - (-10 ) C 4m 500 W L = 0.054m = 54mm < COMMENTS: The corners will cause local departures from one-dimensional conduction and a slightly larger heat loss PROBLEM 1.8 KNOWN: Dimensions and thermal conductivity of food/beverage container Inner and outer surface temperatures FIND: Heat flux through container wall and total heat load SCHEMATIC: ASSUMPTIONS: (1) Steady-state conditions, (2) Negligible heat transfer through bottom wall, (3) Uniform surface temperatures and one-dimensional conduction through remaining walls ANALYSIS: From Fourier’s law, Eq 1.2, the heat flux is $ T2 − T1 0.023 W/m ⋅ K ( 20 − ) C ′′ q =k = = 16.6 W/m L 0.025 m < Since the flux is uniform over each of the five walls through which heat is transferred, the heat load is q = q′′ × A total = q′′  H ( 2W1 + 2W2 ) + W1 × W2  q = 16.6 W/m2  0.6m (1.6m + 1.2m ) + ( 0.8m × 0.6m ) = 35.9 W < COMMENTS: The corners and edges of the container create local departures from onedimensional conduction, which increase the heat load However, for H, W1, W2 >> L, the effect is negligible PROBLEM 1.9 KNOWN: Masonry wall of known thermal conductivity has a heat rate which is 80% of that through a composite wall of prescribed thermal conductivity and thickness FIND: Thickness of masonry wall SCHEMATIC: ASSUMPTIONS: (1) Both walls subjected to same surface temperatures, (2) Onedimensional conduction, (3) Steady-state conditions, (4) Constant properties ANALYSIS: For steady-state conditions, the conduction heat flux through a one-dimensional wall follows from Fourier’s law, Eq 1.2, q ′′ = k ∆T L where ∆T represents the difference in surface temperatures Since ∆T is the same for both walls, it follows that L1 = L2 k1 q ′′ ⋅ k2 q1′′ With the heat fluxes related as q1′′ = 0.8 q ′′2 L1 = 100mm 0.75 W / m ⋅ K × = 375mm 0.25 W / m ⋅ K 0.8 < COMMENTS: Not knowing the temperature difference across the walls, we cannot find the value of the heat rate PROBLEM 1.10 KNOWN: Thickness, diameter and inner surface temperature of bottom of pan used to boil water Rate of heat transfer to the pan FIND: Outer surface temperature of pan for an aluminum and a copper bottom SCHEMATIC: ASSUMPTIONS: (1) One-dimensional, steady-state conduction through bottom of pan ANALYSIS: From Fourier’s law, the rate of heat transfer by conduction through the bottom of the pan is T −T q = kA L Hence, T1 = T2 + qL kA where A = π D2 / = π (0.2m ) / = 0.0314 m Aluminum: T1 = 110 $C + Copper: T1 = 110 $C + 600W ( 0.005 m ) ( 240 W/m ⋅ K 0.0314 m 600W (0.005 m ) ( 390 W/m ⋅ K 0.0314 m2 ) ) = 110.40 $C = 110.25 $C COMMENTS: Although the temperature drop across the bottom is slightly larger for aluminum (due to its smaller thermal conductivity), it is sufficiently small to be negligible for both materials To a good approximation, the bottom may be considered isothermal at T ≈ 110 °C, which is a desirable feature of pots and pans

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