Consider irrotational flow past a stationary sphere of radius R located at the origin. In the limit r→ ∞, the velocity field v = = U2, as in Fig. 8-6 in the book. (a) Calculate the velocity field v assuming potential flow given by v = Vo(r, 0, 0), where the potential can be assumed to be independent of the azimuthal coordinate and v=0. Here, since Ә rde ə V₁ = - U cos and ve Ər for large r/R, look for solutions of the form = f(r) cos 0. Assume a no-penetration boundary condition at the surface of the sphere. (b) Calculate the pressure P and the drag force due to pressure. -U sin 0

Elements Of Electromagnetics
7th Edition
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Author:Sadiku, Matthew N. O.
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Consider irrotational flow past a stationary sphere of radius R located at the
origin. In the limit r→∞, the velocity field v = U2, as in Fig. 8-6 in the
book.
(a) Calculate the velocity field v assuming potential flow given by v =
Vo(r, 0, 0), where the potential can be assumed to be independent
of the azimuthal coordinate and vo= 0. Here, since
ə
rde
Ə
Ər
for large r/R, look for solutions of the form = f(r) cos 0. Assume a
no-penetration boundary condition at the surface of the sphere.
(b) Calculate the pressure P and the drag force due to pressure.
Vr =
U cos 0 and Vo =
-U sin 0
Transcribed Image Text:Consider irrotational flow past a stationary sphere of radius R located at the origin. In the limit r→∞, the velocity field v = U2, as in Fig. 8-6 in the book. (a) Calculate the velocity field v assuming potential flow given by v = Vo(r, 0, 0), where the potential can be assumed to be independent of the azimuthal coordinate and vo= 0. Here, since ə rde Ə Ər for large r/R, look for solutions of the form = f(r) cos 0. Assume a no-penetration boundary condition at the surface of the sphere. (b) Calculate the pressure P and the drag force due to pressure. Vr = U cos 0 and Vo = -U sin 0
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