A flat plate with sharp leading edge is placed in the test section of a low-speed wind tunnel. The working section of the wind tunnel has been designed to produce a region of constant free stream velocity (i.e., for x < 1.0 m, U, = 27.0 m/s), followed by a region of decelerating flow (i.e., for x 2 1.0, U. = A'(1 – m/s, Figure Q1. %3D Wind Tunnel Wal yU. = 27.0.for zS 10m U. m/s, for x2 1.0 m For 1.0m Flat Plate Figure Q1 U, is the freestream air velocity, x is the streamwise position in meter, L,ref is a reference length equal to 10 m and x = 0 corresponds to the leading edge of the flat plate. 1- Determine the constant A and its dimension.

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
8th Edition
ISBN:9781305387102
Author:Kreith, Frank; Manglik, Raj M.
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Chapter5: Analysis Of Convection Heat Transfer
Section: Chapter Questions
Problem 5.30P: Air at 1000C flows at an inlet velocity of 2 m/s between two parallel flat plates spaced 1 cm apart....
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A flat plate with sharp leading edge is placed in the test section of a low-speed wind
tunnel. The working section of the wind tunnel has been designed to produce a region
of constant free stream velocity (i.e., for x < 1.0 m, U̟ = 27.0 m/s), followed by a
region of decelerating flow (i.e., for x 2 1.0, U̟ = A'(1 – m/s, Figure Q1.
Wind Tunnel Wal
- 27.0
0". for xS 1.0 m
m/s.
for x2 1.0 m
For
1.0m
Flat Plate
L.
Figure Q1
U, is the freestream air velocity, x is the streamwise position in meter, Lref is a
reference length equal to 10 m and x = 0 corresponds to the leading edge of the flat
plate.
1- Determine the constant A and its dimension.
Transcribed Image Text:A flat plate with sharp leading edge is placed in the test section of a low-speed wind tunnel. The working section of the wind tunnel has been designed to produce a region of constant free stream velocity (i.e., for x < 1.0 m, U̟ = 27.0 m/s), followed by a region of decelerating flow (i.e., for x 2 1.0, U̟ = A'(1 – m/s, Figure Q1. Wind Tunnel Wal - 27.0 0". for xS 1.0 m m/s. for x2 1.0 m For 1.0m Flat Plate L. Figure Q1 U, is the freestream air velocity, x is the streamwise position in meter, Lref is a reference length equal to 10 m and x = 0 corresponds to the leading edge of the flat plate. 1- Determine the constant A and its dimension.
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