Consider the following fluids at a film temperature of 300 K in parallel flow over a flat plate with velocity of 1 m/s: (1) atmospheric air, (2) water, (3) engine oil, and (4) mercury. For each fluid, determine: (1) Reynolds number (2) boundary layer thicknesses (3) thermal boundary layer thickness at a distance of 40 mm from the leading edge. Assume laminar flow. 5x 8 = 1/2 Rex V · L Re = Prl/3
Consider the following fluids at a film temperature of 300 K in parallel flow over a flat plate with velocity of 1 m/s: (1) atmospheric air, (2) water, (3) engine oil, and (4) mercury. For each fluid, determine: (1) Reynolds number (2) boundary layer thicknesses (3) thermal boundary layer thickness at a distance of 40 mm from the leading edge. Assume laminar flow. 5x 8 = 1/2 Rex V · L Re = Prl/3
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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![Consider the following fluids at a film temperature of 300 K in parallel flow over a
flat plate with velocity of 1 m/s: (1) atmospheric air, (2) water, (3) engine oil, and
(4) mercury.
For each fluid, determine:
(1) Reynolds number (2) boundary layer thicknesses (3) thermal boundary layer
thickness at a distance of 40 mm from the leading edge.
Assume laminar flow.
5x
8 =
1/2
V · L
Re =
Rex
Pr1/3](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fd60d4aee-a131-4a90-92a7-27fe51a2e288%2F6eb7ed4a-abbc-4f65-bcbb-02bed759031b%2Fkak973d_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Consider the following fluids at a film temperature of 300 K in parallel flow over a
flat plate with velocity of 1 m/s: (1) atmospheric air, (2) water, (3) engine oil, and
(4) mercury.
For each fluid, determine:
(1) Reynolds number (2) boundary layer thicknesses (3) thermal boundary layer
thickness at a distance of 40 mm from the leading edge.
Assume laminar flow.
5x
8 =
1/2
V · L
Re =
Rex
Pr1/3
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