ENV5056 Numerical Modeling of Flow and Contaminant Transport in Rivers. Equations. Asst. Prof. Dr. Orhan GÜNDÜZ

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1 ENV5056 Numerical Modeling of Flow and Contaminant Transport in Rivers Derivation of Flow Equations Asst. Prof. Dr. Orhan GÜNDÜZ

2 General 3-D equations of incompressible fluid flow Navier-Stokes Equations General 1-D equations of channel flow (can be simplified from N-S eqns or derived separately) Saint-Venant Equations Further simplifications possible based on dimensionality, time dependency and uniformity of flow 2

3 Three-dimensional Hydrodynamic Equations of Flow The three-dimensional hydrodynamic equations of fluid flow are the basic differential equations describing the flow of a Newtonian fluid. In a three-dimensional cartesiancoordinate system, the conservation of mass equation coupled with the Navier- Stokes equations of motion in x, y and z dimensions form the general hydrodynamic equations. They define a wide range of flow phenomena from unsteady, compressible flows to steady, incompressible flows. 3

4 Three-dimensional Hydrodynamic Equations of Flow Developed by Claude-Louis Navierand George Gabriel Stokes, these equations arise from applying Newton's second law to fluid motion, together with the assumption that the fluid stress is the sum of a diffusing viscous term (proportional to the gradient of velocity), plus a pressure term. Although Navier-Stokes equations only refer to the equations of motion (conservation of momentum), it is commonly accepted to include the equation of conservation of mass. These four equations all together fully describe the fundamental characteristics of fluid motion. 4

5 Some fundamental concepts Velocity vector: v = ui + υ j + wk k j i Unit vectors Dot product of two vectors: [ 1, 2,..., n ] [,,..., ] a = a a a b = b1 b2 bn n a b = a b = a b + a b a b i= 1 i i n n Del operator: = i + j + k x y z 5

6 Some fundamental concepts Gradient of a scalar field, f: f f f f = i + j + k x y z Divergence of a vector field, v: v = ui + υ j + wk div v u υ w = v = + + x y z In Euclidean space, the dot product of two unit vectors is simply the cosine of the angle between them. (Ex: i.i=1x1xcos0=1, i.j=1x1xcos90=0, i.k=1x1xcos90=0) 6

7 Navier-Stokes Equations of Fluid Flow ρ + = t ( ρv) 0 Continuity Equation ρ v + v v = σ + t f Momentum Equation where ρ is fluid density, v is flow velocity vector, σ is stress tensor f is body forces and is del operator. 7

8 Navier-Stokes Equations of Fluid Flow σ τ τ σ τ σ τ τ τ σ xx xy xz = yx yy yz zx zy zz where σ are the normal stresses and τ are shear stresses acting on the fluid 8

9 Navier-Stokes Equations of Fluid Flow Conservation of mass equation: ρ ( ρu) ( ρυ) ( ρw) = t x y z 0 where ρis the density of the fluid, tis time and u, υand ware the components of the velocity vector in x, yand zcoordinates. 9

10 Navier-Stokes Equations of Fluid Flow u u u u σ τ τ t x y z x y z xx yx zx ρ + u + υ + ω = ρ υ υ υ υ τ σ τ u g y t x y z x y z xy yy zy ρ + u + υ + ω = ρ w w w w τ τ σ t x y z x y z xz yz zz ρ + u + υ + ω = ρ g x, g y and g z are gravitational acceleration along x, y and z axes. The terms σ and τare normal and shear stresses acting on the fluid, respectively. The first subscript in the notation indicates the direction of the normal to the plane on which the stress acts, and the second subscript indicates the direction of the stress. g x g z 10

11 Navier-Stokes Equations of Fluid Flow The general equations of motioninclude both velocities and stresses as unknown variables. Using the relationships derived for a compressible Newtonian fluid, one can express the normal and shear stress components in these equations in terms of the velocities: For Newtonian fluids: τ ~ u y Three assumptions needed to define stress terms: 1. The stress tensor is a linear function of the strain rates. 2. The fluid is isotropic. 11

12 Navier-Stokes Equations of Fluid Flow u 2 σ xx = P + 2µ µ v x 3 υ 2 σ yy = P + 2µ µ v y 3 u υ τ xy = τ yx = µ + y x υ w τ yz = τ zy = µ + z y w 2 σ zz = P + 2µ µ v z 3 τ τ µ w u zx = xz = + x z 12

13 Navier-Stokes Equations of Fluid Flow Substituted and simplified: u u u u P u u u 1 u υ w ρ u υ w ρ gx µ µ = t x y z x x y z 3 x x y z υ P 1 u w u υ υ w υ g υ υ υ ρ υ ρ y µ µ υ = t x y z y x y z 3 y x y z w w w w P w w w 1 u υ w ρ u υ w ρ gz µ µ = t x y z z x y z 3 z x y z 13

14 Incompressible Newtonian Fluid Most fluids of practical importance such as water are incompressible, which means that their densities are constant for a wide range of flows. This is a reasonable assumption except for certain extreme situations such as the cases where the fluid is under profound pressures. Since the density of fluid is constant, the continuity equation for incompressible flows can be simplified as: u υ w + + = x y z 0 14

15 Navier-Stokes Equations of Fluid Flow (Incompressible Flow of Newtonian Fluids) u u u u p u u u ρ + u + v + w = + ρ g µ x t x y z x x y z u v v v p v v v ρ + u + v + w = + ρ g y + µ t x y z y x y z u w w w p w w w ρ + u + v + w = + ρ gz + µ t x y z z x y z 15

16 Navier-Stokes Equations of Fluid Flow (Incompressible Flow of Newtonian Fluids) v = 0 Continuity Equation v 2 v v v ρ + = p + ρ g + µ t Momentum Equation Unsteady Acceleration Convective Acceleration Pressure Gradient Other body forces Viscosity 16

17 Saint-Venant Equations of Channel Flow The flow of water through stream channels is a distributed process since the flow rate, velocity and depth vary spatially throughout the channel. Estimates of flow rate or water level at certain locations in the channel system may be obtained using a set of equations that define the conservation of mass and momentum along this channel. This type of a model is based on partial differential equations that allow the flow rate and water level to be computed as a function of space and time. 17

18 Saint-Venant Equations of Channel Flow From a theoretical standpoint, the true flow process in the river system varies in all three spatial coordinate directions (longitudinal, lateral and transverse) as well as time. If a three-dimensional system is used, the resulting equations (modified Navier-Stokes equations for channel flow) would be very complex, and would require considerable amount of field data, which is also spatially variable. In field applications, most of this data could only be described approximately, thus rendering the three dimensional solutions susceptible to data errors. 18

19 Saint-Venant Equations of Channel Flow However, for most practical purposes, the spatial variations in lateral and transverse directions can be neglected and the flow in a river system can be approximated as a one-dimensional process along the longitudinal direction (i.e., in the direction of flow). The Saint Venant equations that were derived in the early 1870s by Barrede Saint-Venant, may be obtained through the application of control volume theory to a differential element of a river reach. The Navier-Stokes equations can be simplified for one-dimensional flow. However, it is more intuitive if these equations are derived from an elemental volume of fluid along a channel. 19

20 Assumptions made in derivation of Saint-Venant Equations of Channel Flow 1. The flow is one-dimensional. The water depth and flow velocity vary only in the direction of flow. Therefore, the flow velocity is constant and the water surface is horizontal across any section perpendicular to the direction of flow. 2. The flow is assumed to vary gradually along the channel so that the hydrostatic pressure distribution prevails and vertical accelerations can be neglected. 3. The channel bottom slope is small. 20

21 Assumptions made in derivation of Saint-Venant Equations of Channel Flow 4. The channel bed is stable such that there is no change in bed elevations in time. 5. The Manning and Chezy equations, which are used in the definition of channel resistance factor in steady, uniform flow conditions, are also used to describe the resistance to flow in unsteady, non-uniform flow applications. 6. The fluid is incompressible and of constant density throughout the flow. 21

22 Cross-sectional view(x-z plane) 22

23 Plan view(x-y plane) Cross-sectional view (Y-Z plane) 23

24 Reynolds Transport Theorem The equations of mass and momentum conservation can be derived starting from the Reynolds Transport Theorem. If B sys and bare defined as extensive and intensive parameters of the system, respectively, the Reynolds Transport Theorem for a fixed non-deforming control volume can be stated as DB sys = ρbd + ρb( V n ) da Dt t cv where ρ and are density and volume of fluid. V is velocity vector. n is the unit vector normal to the control surface and t is time. In this equation, the intensive parameter is defined as extensive property per unit mass. Therefore, if mass is the extensive property, the intensive property becomes unity. cs 24

25 Continuity Equation(Conservation of Mass) The continuity equation can be obtained by simplifying the Reynolds Transport Theorem with the extensive property being the mass of the system. Since the total mass in a system is always constant, the left hand-side of equation becomes zero: 0 = ρd + ρ ( V n) da t cv cs This implies that the time rate of change of mass in the control volume is equal to the difference in cumulative mass inflow and outflow from the control surfaces of the control volume. 25

26 Continuity Equation(Conservation of Mass) Rate of change of mass = Mass inflow Mass outflow This general equation of continuity can be given for the particular case of an open channel with an irregular geometry. As seen in figure, the inflow to the control volume is the sum of the flow Qentering the control volume at the upstream end of the channel and the lateral inflow qentering the control volume as a distributed flow along the side of the channel. In this case, the lateral inflow has the dimensions of flow per unit length of channel. 26

27 Continuity Equation(Conservation of Mass) ρ( Q + qdx) ρ( Q + Q dx) = x ( ρ Adx) t Applying the assumption of constant density and rearranging produces the conservation form of the continuity equation, which is valid for any irregular cross section A Q + q = t x 0 27

28 Momentum Equation It is stated in the Newton's second law for a system that the time rate of change of the linear momentum of the system is equal to the sum of the external forces acting on the system. Using this law in the Reynolds Transport Theorem yields F ρvd ρv ( = + V n) da t cv cs In this case, the intensive property is the velocity of the fluid. This equation reveals that the sum of the forces applied on the system is equal to the time rate of change of momentum stored within the control volume plus the net flow of momentum across the control surfaces 28

29 Momentum Equation For an open channel flow, there are five different forces acting on the control volume: 1. the gravity force along the channel due to weight of water (F g ) 2. the pressure force (F p ) 3. the friction force along the bottom and sides of the channel (F f ) 4. the contraction/expansion force due to abrupt changes in channel cross section (F e ) 5. the wind shear force (F w ) F = F + F + F + F + F g p f e w 29

30 Momentum Equation Gravity Force: The gravity force acting on the control volume shown in figureis a function of the volume of the fluid, which may be given as d = Adx The corresponding weight of the fluid can be expressed as W = ρd g = ρ gadx where gis the gravitational acceleration. The component of weight in the direction of flow becomes the gravity force Fg = ρ gadxsinθ where θis the angle of inclination of the channel bed. With the assumption of a small angle of inclination of the channel bed, the sine of the angle can be approximated as the tangent of the angle: 30

31 Momentum Equation sin( θ ) tan( θ ) which is also equal to the slope of the channel bed, S o. Therefore, for a small angle of inclination of the channel bed, gravity force acting on the control volume can be written as F g = ρ gadxs o 31

32 Momentum Equation Pressure Force: The pressure force is the resultant of the hydrostatic force on the left side of the control volume (F pl ), the hydrostatic force on the right side of the control volume (F rl ) and the pressure force exerted by the banks on the control volume (F pb ) as can be seen from Figure 1.b: F = F F + p pl pr F pb If an element of fluid of thickness dwat an elevation of wfrom the bottom of the channel is immersed at depth y-w, the incremental hydrostatic pressure on this element is computed as ρg(y-w). The corresponding incremental hydrostatic force is then calculated as 32

33 Momentum Equation pl ( ) df = ρ g y w bdw where bis the width of the element across the channel. Integrating this force over the cross section gives the total hydrostatic force on the left end of the control volume pl y 0 ( ) F = ρg y w bdw Using the Taylor's series expansion of the hydrostatic force on the left end, F pl, and ignoring the higher order terms, one might obtain the hydrostaticforceontherightendofthecontrolvolumeas: F pl Fpr = Fpl + dx x 33

34 Momentum Equation The differential of F pl with respect to xin the above equation is computed using the Leibnitz rule for differentiation 0 ( ρ ( ) ) y F g y w b pl dy d0 = dw + ρ g ( y y) b + ρg ( y 0) b x x dx dx where the second and third terms on the right hand-side of the equationare evaluated as zero. The partial derivative term can be expanded using the multiplication rule of differentiation and the differential of F pl with respect to xtakes the following form y y Fpl y b = ρg bdw + ρg ( y w) dw x x x

35 Momentum Equation The first integral in above equation can be simplified as y y y y ρg bdw = ρg bdw = ρg A x x x 0 0 y since A = y 0 bdw The pressure force exerted by the banks on the control volume is related to the rate of change of the width of the channel through the element dxand is given as y b Fpb = ρ g ( y w) dw dx x 0 35

36 Momentum Equation Substituting: F F F = F F + dx + F = dx + F x x pl pl p pl pl pb pb y y y b b Fp = ρg A ρg( y w) dw dx ρ + + g( y w) dw dx x x x 0 0 The resultant pressure force acting on the control volume can be written as: y Fp = ρ g Adx x 36

37 Momentum Equation Friction Force: The friction forces created by shear stress along the bottom and sides of the control volume can be defined in terms of the bed shear stress τ o and can be given as -τ o Pdx, where Pis the wetted perimeter. In accordance with the assumptions stated previously, the bed shear stress can be defined in terms of the steady uniform flow formula: τ = ρgrs = ρg( A/ P) S o f f where Ris the hydraulic radius defined by the ratio of the flow area and the wetted perimeter ands f is the friction slope, which is derived from the Manning's equation and given as 37

38 Momentum Equation 2 n V S f = 2 µ R 2 4 / 3 nis the Manning's roughness coefficient, Vis the flow velocity and µis a constant, which is equal to 1.49 in British units and 1.0 in SI units. Based on the definition of bed shear stress given in aboveequation, the friction force acting on the control volume takes the final form given below F f = ρgas f dx 38

39 Momentum Equation Contraction/Expansion Force: Abrupt contraction or expansion of the channel causes energy loss through turbulence. These losses can be considered similar to the losses in a pipe system. The magnitude of these losses is a function of the change in velocity head, V 2 /2g=(Q/A) 2 /2g, through the length of the channel. The forces associated with these eddy losses can be defined similar to friction force except the term S f is replaced by S e, which is the eddy loss slope representing the loss of energy due to an abrupt contraction or expansion S e = K ec 2g ( Q / A) x 2 where K ec is the non-dimensional expansion or contraction coefficient that is defined as negative for channel expansion and positive for channel contraction. Therefore, contraction/expansion force term becomes: F e = ρgas e dx 39

40 Momentum Equation Wind Shear Force: The wind shear force is caused by the frictional resistance of wind against the free surface of the water. It can be defined as a function of wind shear stress, τ w, and written as τ w Bdx. The wind shear stress is defined as the product of a wind shear factor, W f and fluid density τ w = ρw f W = f C f V r 2 V r where C f is a shear stress coefficient and V r is the velocity of fluid relative to the boundary, which can be written as 40

41 Momentum Equation V Q = A r V w cosω V w is the wind velocity and ωis the angle that wind direction makes with the direction of average fluid velocity, (Q/A). Based on the definition of wind shear stress given in aboveequation,the wind shear force acting on the control volume takes the final form given below F w = ρw f Bdx Finally, the sum of the five forces define the total force on the left-hand side of the momentum equation F = ρgas o dx ρga y x dx ρgas f dx ρgas e dx ρw Bdx f 41

42 Momentum Equation F ρvd ρv ( = + V n) da t cv The two momentum terms on the right-hand side represent the rate of change of storage of momentum in the control volume and the net outflow of momentum across the control surface, respectively The net momentum outflow is the sum of momentum outflow minus the momentum inflow to the control volume. The mass inflow rate to the control volume is the sum of both stream inflow and the lateral inflow and is defined as -ρ(q + qdx). cs 42

43 Momentum Equation The momentum inflow to the control volume is computed by multiplying the two mass inflow rates by their respective velocities and a momentum correction factor, β: V ρ( V n) da = ρ( βvq + βυxqdx) inlet where υ x is the average velocity of lateral inflow in the direction of main channel flow. The momentum coefficient, β, accounts for the non-uniform distribution of velocity at a specific channel cross section. 1 2 β = υ da 2 V A where υis the velocity of the fluid in a small elemental area dain the channel cross section. Generally, the value of the momentum coefficient ranges from 1.01 for straight prismatic channels to 1.33 for river valleys with floodplains 43

44 Momentum Equation The momentum outflow from the control volume is also a function of mass outflow from the control volume, which can be defined as the Taylor series expansion of mass inflow. Hence, the momentum outflow from the control volume is computed as: βvq ( β ) V ρ( V n) da = ρ βvq + dx x outlet Thus, net momentum outflow across the control surface ( βvq) ( βvq) V ρ( V n) da = ρ ( βvq + βυxqdx) + ρ βvq + dx = ρ βυxq dx x x cs 44

45 Momentum Equation The time rate of change of momentum stored in the control volume is written as a function of the volume of the elemental channel length dx. The momentum associated with this elemental volume can be written as ρvadx, or ρqdxand the time rate of change of momentum is given as t Q V ρ d = ρ dx t cv When all terms are combined and substituted back into the momentum equation: F ρvd ρv ( = + V n) da t cv cs ρgas o dx ρga y x dx ρgas f dx ρgas e dx W Bρdx f = ρ βυ xq ( βvq) dx x Q + ρ t dx 45

46 Momentum Equation Thisequationis simplified and rearranged to the following form if all terms are divided by ρdxand Vis replaced by Q/A 0 2 = W B q S S S x y ga x A Q t Q f x e f o υ β β ) / ( 46 x x t The waterdepth termin thisequationcan be replaced by the water surface elevation (stage), h, using the equality z y h + = where zis the channel bottom above a datum such as mean sea level as seen in figure. The derivative of thiswith respect to xis written as x z x y x h + =

47 Momentum Equation However, the term z/xis equal to the negative of the slope of the channel, so theequationcan also be written as S o x y x h = The momentum equation can now be expressed in terms of hby 47 The momentum equation can now be expressed in terms of hby 0 2 = W B q S S x h ga x A Q t Q f x e f υ β β ) / (

48 Saint-Venant Equations The continuity and momentum equations are always addressed together and form the conservation form of the Saint-Venant equations 0 = + q x Q t A = W B q S S x h ga x A Q t Q f x e f υ β β ) / ( These equations are the governing equations of one-dimensional unsteady flow in open channels and were originally developed by the French scientist Barrede Saint-Venantin 1872

49 Saint-Venant Equations Steady State Under steady state assumption, Saint-Venant equations simplify to: dq q dx = 0 β dx 2 d( Q / A) dh + ga + S f + Se βqυ x + Wf B = dx 0 49

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