Fundamentals of Aerodynamics
Fundamentals of Aerodynamics
6th Edition
ISBN: 9781259129919
Author: John D. Anderson Jr.
Publisher: McGraw-Hill Education
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Chapter 3, Problem 3.21P

Consider the streamlines over a circular cylinder as sketched at the right of Figure 3.26. Single out the first three streamlines flowing over the top of the cylinder. Designate each streamline by its stream function, ψ 1 , ψ 2 and ψ 3 . The first streamline wets the surface of the cylinder: designate ψ 1 = 0 . The streamline above that is ψ 2 and the next one above that is ψ 3 . Assume the streamlines start out in the freestream equally spaced. Hence, the volume flow rates between the streamlines are the same. The streamline ψ 2 passes through the point ( 1.2 R , π / 2 ) directly above the top of the cylinder. Calculate the location of the point directly above the top of the cylinder through which the streamline ψ 3 flows. Comment on the spacing between the streamlines directly above the top.

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The figure below shows 4 streamlines corresponding to a free vortex flow. The streamlines are concentric eircles, and the velocity magnitude Valong each streamline is given by V = K/r, where r is the radial distance from the center, and K is a constant. Assume the flow to be steady, incompressible and inviscid. Neglect the effects of gravity. If K = 20 m2/s and the fluid density is 1000 kg/m, what is the magnitude of the static pressure difference AP between 2 streamlines at radial distances r = 3 m and r = 4 m? Ap = 1 КРа. C r В
(а) A two-dimensional flow field in the xy plane is given by u = v = x2+y2 x2+y2 where u and v are the velocity components in the x and y directions, respectively and K is a positive constant. Determine the equations for the streamlines. Plot the velocity field, and streamlines on the same figure (You may hand plot or computer plot). Show any FIVE streamlines and label the streamlines in a positive x-y region (you may choose a suitable range). Discuss the important features of the plots.
Consider a velocity field where the x and y components of velocity are given by u = cx and v = -cy, where c is a constant. Obtain the equations of the streamlines.

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