The radial velocity component in an incompressible, two- dimensional flow field (v, = 0) is 5- %3D v, = 2r + 31² sin 0 Determine the corresponding tangential velocity component, vg, required to satisfy conservation of mass.
The radial velocity component in an incompressible, two- dimensional flow field (v, = 0) is 5- %3D v, = 2r + 31² sin 0 Determine the corresponding tangential velocity component, vg, required to satisfy conservation of mass.
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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![• Y:EA
09B/s
* etisalat
sheet 2.pdf
->
The radial velocity component in an incompressible, two-
dimensional flow field (v, = 0) is
5-
v, = 2r + 31² sin 0
Determine the corresponding tangential velocity component, vg,
required to satisfy conservation of mass.
If the velocity field is given by V = axri – ayj, and a is a con-
stant, find the circulation around the closed curve shown in Fig. 2 .
6-
(1, 2)
(2, 2)
(1, 1)
(2, 1)
Fig. 2
Damietta University
Faculty of Engineering
Mechanical Engineering Department
Fluid Mechanics II
7-
For a steady, two-dimensional, incompressible flow, the ve-
locity is given by V = (ax – cy)i + (-ay + cx)j, where a and c
are constants. Show that this flow can be considered inviscid.
Determine the shearing stress for an incompressible Newtonian
31
8-](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F39fd94ae-059a-488c-95d5-39bd94a1a576%2Fb0f47a94-d20d-4a3a-9b67-31c258b2ac81%2Fnohbt6x_processed.png&w=3840&q=75)
Transcribed Image Text:• Y:EA
09B/s
* etisalat
sheet 2.pdf
->
The radial velocity component in an incompressible, two-
dimensional flow field (v, = 0) is
5-
v, = 2r + 31² sin 0
Determine the corresponding tangential velocity component, vg,
required to satisfy conservation of mass.
If the velocity field is given by V = axri – ayj, and a is a con-
stant, find the circulation around the closed curve shown in Fig. 2 .
6-
(1, 2)
(2, 2)
(1, 1)
(2, 1)
Fig. 2
Damietta University
Faculty of Engineering
Mechanical Engineering Department
Fluid Mechanics II
7-
For a steady, two-dimensional, incompressible flow, the ve-
locity is given by V = (ax – cy)i + (-ay + cx)j, where a and c
are constants. Show that this flow can be considered inviscid.
Determine the shearing stress for an incompressible Newtonian
31
8-
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