6- A uniform free stream of air at 0.8 m/s flows over a flat plate (4 m long x 1 m wide). Assuming the boundary layer to be laminar on the plate and the velocity profile is: и y Find the ratio of the drag force on the front half portion to the drag %3D U 28 28 force on the rear half portion of the plate. (p = 1.2 kg/m³ ; v = 1.51×10$ m³/s) [2.42]
6- A uniform free stream of air at 0.8 m/s flows over a flat plate (4 m long x 1 m wide). Assuming the boundary layer to be laminar on the plate and the velocity profile is: и y Find the ratio of the drag force on the front half portion to the drag %3D U 28 28 force on the rear half portion of the plate. (p = 1.2 kg/m³ ; v = 1.51×10$ m³/s) [2.42]
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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![6- A uniform free stream of air at 0.8 m/s flows over a flat plate (4 m long x 1 m wide).
Assuming the boundary layer to be laminar on the plate and the velocity profile is:
и
Find the ratio of the drag force on the front half portion to the drag
%3D
U
force on the rear half portion of the plate. (p = 1.2 kg/m ; v= 1.51×10* m³/s)
[2.42]](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F86cd17be-79cd-447c-b847-4cef9b7c15c4%2F9ab41650-9838-49fe-98b1-f4246d92513b%2F3qtpc7o_processed.jpeg&w=3840&q=75)
Transcribed Image Text:6- A uniform free stream of air at 0.8 m/s flows over a flat plate (4 m long x 1 m wide).
Assuming the boundary layer to be laminar on the plate and the velocity profile is:
и
Find the ratio of the drag force on the front half portion to the drag
%3D
U
force on the rear half portion of the plate. (p = 1.2 kg/m ; v= 1.51×10* m³/s)
[2.42]
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