Source flow:It is type of flow,where all the streamlines are straight lines emanating from a central point.The velocity along each of the streamlines vary inversely with distance from central point.Velocity components in the radial and tangential directions are VrandVθ.Vr=Λ2πrΛ=sourcestrengthVθ=0
Example:For a source flow ,calculate
(a).The time rate of change of the volume of a fluid element per unit volume.
(b) The vorticity.
(b) The vorticity.
Solution : (a)∇.→V=1∂VD(∂V)Dt
In polar-coordinates we have ∇.→V=1r∂∂r(rVr)+1r∂Vθ∂θ
Letx=rcosθy=rsinθVr=ucosθ+vsinθVθ=−usinθ+vcosθ
Let velocity field is given byu=cx(x2+y2)=crcosθr2=ccosθrv=cy(x2+y2)=crsinθr2=csinθr
thereforeVr=crcos2θ+crsin2θ=crVθ=−crcosθsinθ+crcosθsinθ=0∇.→V=1r∂(c)∂r+1r∂(0)∂θ=0
(b) Vorticity is given by∇×→V=ez[∂Vθ∂r+Vθr−1r∂Vr∂θ]∇×→V=ez[0+0−0]=0
Therefore, the flow field is ir-rotational.
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