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Two-dimensional flow
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<h2 id="flow-velocity-in-two-dimensional-flows">Flow velocity in two dimensional flows</h2> <h3>Flow velocity in Cartesian co-ordinates</h3> <p>Considering a two dimensional flow in the X − Y {\displaystyle X-Y} plane, the flow velocity at any point ( x , y , z ) {\displaystyle (x,y,z)} at time t {\displaystyle t} can be expressed as – </p> v ¯ ( x , y , z , t ) = v x ( x , y , z , t ) i ^ + v y ( x , y , z , t ) j ^ . {\displaystyle {\bar {\boldsymbol {v}}}(x,y,z,t)=v_{x}(x,y,z,t){\hat {\boldsymbol {i}}}+v_{y}(x,y,z,t){\hat {\boldsymbol {j}}}.} <h3>Velocity in cylindrical co-ordinates</h3> <p>Considering a two dimensional flow in the r − θ {\displaystyle r-\theta } plane, the flow velocity at a point ( r , θ , z ) {\displaystyle (r,\theta ,z)} at a time t {\displaystyle t} can be expressed as – </p> v ¯ ( r , θ , z , t ) = v r ( r , θ , z , t ) r ^ + v θ ( r , θ , z , t ) θ ^ . {\displaystyle {\bar {\boldsymbol {v}}}(r,\theta ,z,t)=v_{r}(r,\theta ,z,t){\hat {\boldsymbol {r}}}+v_{\theta }(r,\theta ,z,t){\hat {\boldsymbol {\theta }}}.} <h2 id="vorticity-in-two-dimensional-flows">Vorticity in two dimensional flows</h2> <h3>Vorticity in Cartesian co-ordinates</h3> <p><a href="/facts/Vorticity/2oQ6eT4d">Vorticity</a> in two dimensional flows in the X − Y {\displaystyle X-Y} plane can be expressed as – </p> ω ¯ = ω z k ^ , {\displaystyle {\bar {\boldsymbol {\omega }}}=\omega _{z}{\hat {\boldsymbol {k}}},} ω z = ∂ v y ∂ x − ∂ v x ∂ y . {\displaystyle \omega _{z}={\frac {\partial v_{y}}{\partial x}}-{\frac {\partial v_{x}}{\partial y}}.} <h3>Vorticity in cylindrical co-ordinates</h3> <p><a href="/facts/Vorticity/2oQ6eT4d">Vorticity</a> in two dimensional flows in the r − θ {\displaystyle r-\theta } plane can be expressed as – </p> ω ¯ = ω z k ^ {\displaystyle {\bar {\boldsymbol {\omega }}}=\omega _{z}{\hat {\boldsymbol {k}}}} ω z = 1 r ∂ ∂ r ( r ∂ ψ ∂ r ) + 1 r 2 ∂ 2 ψ ∂ r 2 . {\displaystyle \omega _{z}={\frac {1}{r}}{\frac {\partial }{\partial r}}(r{\frac {\partial \psi }{\partial r}})+{\frac {1}{r^{2}}}{\frac {\partial ^{2}\psi }{\partial r^{2}}}.} <h2 id="two-dimensional-sources-and-sinks">Two dimensional sources and sinks</h2> <h3>Line/point source</h3> <p>A line source is a line from which fluid appears and flows away on planes perpendicular to the line. When we consider 2-D flows on the perpendicular plane, a line source appears as a point source. By symmetry, we can assume that the fluid flows radially outward from the source. The strength of a source can be given by the <a href="/facts/Volume_flow_rate/X5KI7zzH">volume flow rate</a> Q {\displaystyle Q} that it generates. </p> <h3>Line/point sink</h3> <p>Similar to a line source, a line sink is a line which absorbs fluid flowing towards it, from planes perpendicular to it. When we consider 2-D flows on the perpendicular plane, it appears as a point sink. By symmetry, we assume the fluid flows radially inwards towards the sink. The strength of a sink is given by the volume flow rate Q {\displaystyle Q} of the fluid it absorbs. </p> <h2 id="types-of-two-dimensional-flows">Types of two-dimensional flows</h2> <h3>Uniform source flow</h3> <p>A <a href="/facts/Axisymmetric/bpvJqcnS">radially symmetrical</a> flow field directed outwards from a common point is called a source flow. The central common point is the line source described above. Fluid is supplied at a constant rate Q {\displaystyle Q} from the source. As the fluid flows outward, the area of flow increases. As a result, to satisfy <a href="/facts/Continuity_equation/GVav2Vet">continuity equation</a>, the velocity decreases and the <a href="/facts/Streamlines%2c_streaklines%2c_and_pathlines/sLb4nHR1">streamlines</a> spread out. The velocity at all points at a given distance from the source is the same. </p> <p>The velocity of fluid flow can be given as - </p> v ¯ = v r ( r ) e ^ r . {\displaystyle {\bar {\boldsymbol {v}}}=v_{r}(r){\hat {\boldsymbol {e}}}_{r}.} <p>We can derive the relation between <a href="/facts/Volumetric_flow_rate/X5KI7zzH">flow rate</a> and velocity of the flow. Consider a cylinder of unit height, coaxial with the source. The rate at which the source emits fluid should be equal to the rate at which fluid flows out of the surface of the cylinder. </p> ∫ S v ¯ ⋅ d S ¯ = 2 π r v r ( r ) = Q , {\displaystyle \int \limits _{S}{\bar {\boldsymbol {v}}}\cdot {d{\bar {\boldsymbol {S}}}}=2\pi rv_{r}(r)=Q,} ∴ v r ( r ) = Q 2 π r . {\displaystyle \therefore \;\;v_{r}(r)={\frac {Q}{2\pi r}}.} <p>The <a href="/facts/Stream_function/nEoYTGAl">stream function</a> associated with source flow is – </p> ψ ( r , θ ) = Q 2 π θ . {\displaystyle \psi (r,\theta )={\frac {Q}{2\pi }}\theta .} <p>The <a href="/facts/Steady_flow/y7uzSCfg">steady flow</a> from a point source is irrotational, and can be derived from <a href="/facts/Velocity_potential/9co8hU9D">velocity potential</a>. The velocity potential is given by – </p> ϕ ( r , θ ) = Q 2 π ln r . {\displaystyle \phi (r,\theta )={\frac {Q}{2\pi }}\ln r.} <h3>Uniform sink flow</h3> <p>Sink flow is the opposite of source flow. The streamlines are radial, directed inwards to the line source. As we get closer to the sink, area of flow decreases. In order to satisfy the <a href="/facts/Continuity_equation/GVav2Vet">continuity equation</a>, the <a href="/facts/Streamlines%2c_streaklines%2c_and_pathlines/sLb4nHR1">streamlines</a> get bunched closer and the velocity increases as we get closer to the source. As with source flow, the velocity at all points equidistant from the sink is equal. </p> <p>The velocity of the flow around the sink can be given by – </p> v ¯ = − v r ( r ) e ^ r , {\displaystyle {\bar {\boldsymbol {v}}}=-v_{r}(r){\hat {\boldsymbol {e}}}_{r},} v r ( r ) = Q 2 π r . {\displaystyle v_{r}(r)={\frac {Q}{2\pi r}}.} <p>The <a href="/facts/Stream_function/nEoYTGAl">stream function</a> associated with sink flow is – </p> ψ ( r , θ ) = − Q 2 π θ . {\displaystyle \psi (r,\theta )=-{\frac {Q}{2\pi }}\theta .} <p>The flow around a line sink is irrotational and can be derived from velocity potential. The velocity potential around a sink can be given by – </p> ϕ ( r , θ ) = − Q 2 π ln r . {\displaystyle \phi (r,\theta )=-{\frac {Q}{2\pi }}\ln r.} <h3>Irrotational vortex</h3> <p>A <a href="/facts/Vortex/K6oeqcuX">vortex</a> is a region where the fluid flows around an imaginary axis. For an irrotational vortex, the flow at every point is such that a small particle placed there undergoes pure <a href="/facts/Translation/2foI82so">translation</a> and does not rotate. Velocity varies inversely with radius in this case. Velocity will tend to inf {\displaystyle \inf } at r = 0 {\displaystyle r=0} that is the reason for center being a singular point. The velocity is mathematically expressed as – </p> v = v θ e ^ θ , {\displaystyle {\boldsymbol {v}}=v_{\theta }{\hat {\boldsymbol {e}}}_{\theta },} v θ = K 2 π r . {\displaystyle v_{\theta }={\frac {K}{2\pi r}}.} <p>Since the fluid flows around an axis, </p> v r = 0. {\displaystyle v_{r}=0.} <p>The stream function for <a href="/facts/Irrotational_vortices/K6oeqcuX">irrotational vortices</a> is given by – </p> ψ = − K 2 π ln r . {\displaystyle \psi =-{\frac {K}{2\pi }}\ln r.} <p>While the velocity potential is expressed as – </p> ϕ = − K 2 π θ . {\displaystyle \phi =-{\frac {K}{2\pi }}\theta .} <p>For the closed curve enclosing origin, circulation (line integral of velocity field) Γ = K {\displaystyle \Gamma =K} and for any other closed curves, Γ = 0 {\displaystyle \Gamma =0} </p> <h3>Doublet</h3> <p>A doublet can be thought of as a combination of a source and a sink of equal strengths kept at an infinitesimally small distance apart. Thus the streamlines can be seen to start and end at the same point. The strength of a doublet made by a source and sink of strength Q {\displaystyle Q} kept a distance d s {\displaystyle ds} is given by – </p> Λ = Q d s 2 π . {\displaystyle \Lambda =Q{\frac {ds}{2\pi }}.} <p>The velocity of fluid flow can be expressed as – </p> v = v r e ^ r + v θ e ^ θ , {\displaystyle {\boldsymbol {v}}=v_{r}{\hat {\boldsymbol {e}}}_{r}+v_{\theta }{\hat {\boldsymbol {e}}}_{\theta },} v r = − Λ r 2 cos θ , {\displaystyle v_{r}=-{\frac {\Lambda }{r^{2}}}\cos \theta ,} v θ = − Λ r 2 sin θ . {\displaystyle v_{\theta }=-{\frac {\Lambda }{r^{2}}}\sin \theta .} <p>The equations and the plot are for the limiting condition of d s → 0 {\displaystyle ds\rightarrow 0} </p><p>The concept of a doublet is very similar to that of <a href="/facts/Electric_dipole_moment/ou2LDUVg">electric dipoles</a> and <a href="/facts/Magnetic_dipoles/Ny0TVUSX">magnetic dipoles</a> in <a href="/facts/Electrodynamics/oAkmALHT">electrodynamics</a>. </p> <ul><li>Kothandaraman, C. P.; Rudramoorthy, R. (2006), <i>Fluid Mechanics and Machinery</i> (2nd ed.), New Age International, <a href="/facts/ISBN_(identifier)/15AdSPa9">ISBN</a> 978-1906574789</li></ul> <h2 id="external-links">External links</h2> <ul><li><a href="http://farside.ph.utexas.edu/teaching/336L/Fluidhtml/node61.html">Two-dimensional sources and sinks</a></li></ul>