Fundamentals of Heat and Mass Transfer
Fundamentals of Heat and Mass Transfer
7th Edition
ISBN: 9780470917855
Author: Bergman, Theodore L./
Publisher: John Wiley & Sons Inc
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Chapter 7, Problem 7.2P

Engine oil at 100 ° C and a velocity of 0.1 m/s flows over both surfaces of a 1-m-long flat plate maintained at Determine:

  1. The velocity and thermal boundary layer thick-nesses at the trailing edge.
  2. The local heat flux and surface shear stress at the trailing edge.
  3. The total drag force and heat transfer per unit width of the plate.
  4. Plot the boundary layer thicknesses and local values of the surface shear stress, convection coefficient, and heat flux as a function of x for 0 x 1 m .

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Engine oil at 100°C and a velocity of 0.15 m/s flows over both surfaces of a 1.1-m-long flat plate maintained at 20°C. Determine: (a) The velocity and thermal boundary layer thicknesses at the trailing edge. (b) The local heat flux and surface shear stress at the trailing edge. (c) The total drag force and heat transfer per unit width of the plate. Determine the velocity boundary layer thickness & at the trailing edge, in m. 8 = i m Determine the thermal boundary layer thicknesses &, at the trailing edge, in m. 8, = i m Determine the magnitude of the local heat flux at the trailing edge, W/m². q" x = i W/m² Determine the local surface shear stress at the trailing edge, in N/m². Ts, L = i N/m² Determine the total drag force per unit width of the plate, in N/m. D' = i N/m Determine the magnitude of the heat transfer per unit width of the plate, in W/m. q' = W/m i
Engine oil at 100°C and a velocity of 0.20 m/s flows over both surfaces of a 1.1-m-long flat plate maintained at 20°C. Determine: (a) The velocity and thermal boundary layer thicknesses at the trailing edge. (b) The local heat flux and surface shear stress at the trailing edge. (c) The total drag force and heat transfer per unit width of the plate. Determine the velocity boundary layer thickness & at the trailing edge, in m. 8 = i m Determine the thermal boundary layer thicknesses &, at the trailing edge, in m. 8, = i m Determine the magnitude of the local heat flux at the trailing edge, W/m². q" x = i W/m² Determine the local surface shear stress at the trailing edge, in N/m². Ts, L i N/m² Determine the total drag force per unit width of the plate, in N/m. D' = i N/m Determine the magnitude of the heat transfer per unit width of the plate, in W/m. d' = W/m i

Chapter 7 Solutions

Fundamentals of Heat and Mass Transfer

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