2. A two-dimensional flow field for a inviscid, incompressible fluid is described by the velocity components u = Uo + 2y v = 0 where U, is a constant. If the pressure at the origin shown on the figure is determine an expression for the pressure at (a) point A, and (b) point B. Explain clearly how you obtained your answer. Can you sketch streamlines for this flow field? How about equipotential lines? Why/why not. Assume that the units are consistent and body forces may be neglected. Ро, • B(O, 1) A(1, 0) Ро
2. A two-dimensional flow field for a inviscid, incompressible fluid is described by the velocity components u = Uo + 2y v = 0 where U, is a constant. If the pressure at the origin shown on the figure is determine an expression for the pressure at (a) point A, and (b) point B. Explain clearly how you obtained your answer. Can you sketch streamlines for this flow field? How about equipotential lines? Why/why not. Assume that the units are consistent and body forces may be neglected. Ро, • B(O, 1) A(1, 0) Ро
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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![2. A two-dimensional flow field for a inviscid, incompressible fluid is described by the velocity components
u = Uo + 2y
y
v= 0
where U, is a constant. If the pressure at the origin shown on the figure is po,
В(О, 1)
determine an expression for the pressure at (a) point 4, and (b) point B. Explain
clearly how
field? How about equipotential lines? Why/why not. Assume that the units are
consistent and body forces may be neglected.
you obtained
your answer. Can you sketch streamlines for this flow
A(1, 0)
Ро](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F03bab573-3455-4814-8d3d-5268e6401e29%2F556efb04-1b12-4f24-8a48-063fb194c3b3%2Fqdnf8rw_processed.png&w=3840&q=75)
Transcribed Image Text:2. A two-dimensional flow field for a inviscid, incompressible fluid is described by the velocity components
u = Uo + 2y
y
v= 0
where U, is a constant. If the pressure at the origin shown on the figure is po,
В(О, 1)
determine an expression for the pressure at (a) point 4, and (b) point B. Explain
clearly how
field? How about equipotential lines? Why/why not. Assume that the units are
consistent and body forces may be neglected.
you obtained
your answer. Can you sketch streamlines for this flow
A(1, 0)
Ро
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