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Sources and Sinks

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Sources And Sinks


PYQs

Sources And Sinks

1) Two sources, each of strength m, are placed at the point at the points (a,0), (a,0) and a sink of strength 2m at origin. Show that the stream lines are the curves (x2+y2)2= a2(x2y2+λxy), where λ is variable parameter.

Show also that the fluid speed at any point is (2ma2)/(r1r2r3), where r1, r2 and r3 are the distances of the points from the sources and the sink, respectively.

[2019, 20M]

First Part: The complex potential w at any point P(z) is given by w=mlog(za)mlog(z+a)+2mlogz(1)

w=m[logz2log(z2a2)]

ϕ+iψ=m[log(x2y2+2by)log(x2y2a2+2by)], as z=x+iy

2019-8(c)

Equating the imaginary parts, we have ψ=m[tan1{2xy/(x2y2)}tan1{2xy/(x2y2a2)}]ψ=mtan1[2a2xy(x2+y2)2a2(x2y2)], on simplification 

The desired streamlines are given by ψ= constant =mtan1(2/λ). Then we obtain

(2/λ)=(2a2xy)/[(x2+y2)2a2(x2y2)] or (x2+y2)2=a2(x2y2+λxy)

Second Part: We have,

dwdz=mzamz+a+2mz=2a2mz(za)(z+a) q=|dwdz|=2a2m|zvertza||z+a|=2a2mr1r2r3 where r1=|za|,r2=|z+a| and r3=|z|

2) If fluid fills the region of space on the positive side of the xaxis, which is a right boundary and if there be a sources m at the point (0,a) and an equal sink at (0,b) and if the pressure on the negative side be the same as the pressure at infinity, show that the resultant pressure on the boundary is πρm2(ab)2{2ab(a+b)} where ρ is the density of the fluid.

[2013, 15M]

The object system consists of source +m at A (o,a), i-e. at z=ia and sink m at z=ib. The image system consists of source +m at A(z=ia) and sink m at B(z=ib) w.r.t the positive line OX which is rigid boundary.

The complex potential due to object system with rigid boundary is equivalent to the object system and its image system with no rigid boundary.

w=mlog(zia)+mlog(zib)mlog(z+ia)+mlog(z+ib)=mlog(z2+a2)+mlog(z2+b2)

Now, dwdz=2m=[1z2+a21z2+b2]=2mz(a2b2)(z2+a2)(22+b2)q=|dωdz |=2m(a2b2)|z|\vertz2+a2 |\vertz2+b |

For any point on x -axis, we have z=x so that q=2mx(a2b2)(x2+a2)(x2+b2)

This is the expression for velocity at any point on x-axis. Let P0 be the pressure at x=. By Bernoulli equation for steady motion.

Pρ+12q2=c

In view of p=ρ0,q=0 when x= we get c=p0/ρ. P0Pρ=12q2

Required pressure P on boundary is given by:

P=(P0P)dx=12ρq2dx=12ρ4m2x2(a2b2)2(x2+a2)2(x2+b2)2dx=4ρm2(a2b2)20x2dx(x2+a2)2(x2+b2)2=4m2ρ0[a2+b2a2b2{1x2+b21x2+a2}a2(x2+a2)2b2(x2+b2)2]dx.=4m2f[a2+b2a2b2{π2bπ2a}π4aπ4b]=πρm2(ab)2ab(a+b)=4m2f[a2+b2a2b2{π2bπ2a}π4aπ4b]=πρm2(ab)2ab(a+b)

(We have used below results) 0dxx2+a2=[1atanxa]0=π2aAlso ,0dx(x2+a2)2=1a30cos2θdθ;x=atanθ=x42a30π/2(1+cos2θ)dθ=π212a3=π4a3


3) Two sources, each of strength m are placed at the point (a,0), (a,0) and a sink of strength 2m is at the origin. Show that the stream lines are the curves: (x2+y2)2=a2(x2y2+λxy) where λ is a variable parameter. Show also that the fluid speed at any point is (2ma2)/(r1r2r3), where r1r2 and r3 are the distance of the points from the source and the sink.

[2009, 12M]

First Part:

The complex potential w at any point P(z) is given by:

w=mlog(za)mlog(z+a)+2mlogz(1) or, w=m[logz2log(z2a2)] or ϕ+iψ=m[log(x2y2+2ixy)log(x2y2a2+2ixy)], as z=x+iy

Equating the imaginary parts, we have ψ=m[tan1{2xy/(x2y2)}tan1{2xy/(x2y2a2)}]ψ=mtan1[2a2xy(x2+y2)2a2(x2y2)], on simplification. 

The desired streamlines are given by ψ= constant =mtan1(2/λ). Then we obtain (2/λ)=(2a2xy)/[(x2+y2)2a2(x2y2)] or  (x2+y2)2=a2(x2y2+λxy)

Second Part: From (1), we have

dwdz=mzamz+a+2mz=2a2mz(za)(z+a)

q=|dwdz |=2a2m|z||za||z+a|=2a2mr1r2r3, where

r1=|za|, r2=|z+a| and r3=|z|


4) Let the fluid fills the region x0 (right half of d plane). Let a source α be (0,y1) and equal sink at (0,y2),y1>y2. Let the pressure be same as pressure infinity i.e., p0. Show that the resultant pressure on the boundary yaxis is πρα2(y1y2)2/2y1y2(y1+y2), ρ being the density of the fluid.

[2008, 30M]


5) Two sources, each of strength m are placed at the points (a,0) and (a,0) and a sink of strength 2m is placed at the origin. Show that the stream lines are the curves (x2+y2)2=a2(x2y2+λxy), where λ is a variable parameter. Also show that fluid speed at any point is 2ma2r1r2r3 where r1r2 and r1 are respectively the distance of the point from the sources and sink.

[2003, 15M]

First Part:

The complex potential w at any point P(z) is given by:

w=mlog(za)mlog(z+a)+2mlogz(1) or, w=m[logz2log(z2a2)] or ϕ+iψ=m[log(x2y2+2ixy)log(x2y2a2+2ixy)], as z=x+iy

Equating the imaginary parts, we have ψ=m[tan1{2xy/(x2y2)}tan1{2xy/(x2y2a2)}]ψ=mtan1[2a2xy(x2+y2)2a2(x2y2)], on simplification. 

The desired streamlines are given by ψ= constant =mtan1(2/λ). Then we obtain (2/λ)=(2a2xy)/[(x2+y2)2a2(x2y2)] or  (x2+y2)2=a2(x2y2+λxy)

Second Part: From (1), we have

dwdz=mzamz+a+2mz=2a2mz(za)(z+a)

q=|dwdz |=2a2m|z||za||z+a|=2a2mr1r2r3, where

r1=|za|, r2=|z+a| and r3=|z|


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