2. (a) 4 m, a width of 6 m and U = 1.8 m/s. For one side of the plate, find: Air at 40 °C and 1 atm (abs) flows over a sharp edged flat plate with L = (i) The local boundary layer thickness 8(L). (ii) Local skin friction coefficient at x = L, Cr (L). (iii) Local wall shear stress at x = L, Tw(L).
2. (a) 4 m, a width of 6 m and U = 1.8 m/s. For one side of the plate, find: Air at 40 °C and 1 atm (abs) flows over a sharp edged flat plate with L = (i) The local boundary layer thickness 8(L). (ii) Local skin friction coefficient at x = L, Cr (L). (iii) Local wall shear stress at x = L, Tw(L).
Introduction to Chemical Engineering Thermodynamics
8th Edition
ISBN:9781259696527
Author:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Publisher:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Chapter1: Introduction
Section: Chapter Questions
Problem 1.1P
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Transcribed Image Text:2.
Air at 40 °C and 1 atm (abs) flows over a sharp edged flat plate with L =
4 m, a width of 6 m and U» = 1.8 m/s. For one side of the plate,
find:
(a)
(i)
The local boundary layer thickness 8(L).
(ii)
Local skin friction coefficient at x = L, Cr (L).
(iii) Local wall shear stress at x = L, tw(L).
(iv) Drag coefficient over the total plate and Drag force over the total
plate.
(b) A polymer solution (density = 1180 kg/m³) is being pumped at a
rate of 4200 kg/h through an 80 mm inside diameter pipe. The flow
is known to be laminar and the power-law constants for the solution
are m = 3.6 Pa.s (N.s/m²) and n = 0.8.
(i)
Estimate the pressure drop over a 30 m length of straight
pipe
(ii)
Estimate the centre-line velocity.
(iii)
Calculate the Reynolds number.
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