Final Review Ground Water Basics • • • • Porosity Head Hydraulic Conductivity Transmissivity Porosity Basics • Porosity n (or f) n • Volume of pores is also the total volume – the solids volume Vpores Vtotal Vtotal Vsolids n Vtotal • Porosity Basics Vtotal Vsolids Can re-write that as: n Vtotal • Then incorporate: • Solid density: rs = Msolids/Vsolids • Bulk density: rb = Msolids/Vtotal • rb/rs = Vsolids/Vtotal Vsolids n 1 Vtotal rb n 1 rs Porosity Basics • Volumetric water content (q) – Equals porosity for saturated system Vwater q Vtotal Ground Water Flow • • • • • • • Pressure and pressure head Elevation head Total head Head gradient Discharge Darcy’s Law (hydraulic conductivity) Kozeny-Carman Equation Multiple Choice: Water flows…? • Uphill • Downhill • Something else Pressure and Pressure Head • Pressure relative to atmospheric, so P = 0 at water table • P = rghp – r density – g gravity – hp depth Pressure Head (increases with depth below surface) Elevation P = 0 (= Patm) Head Elevation Head • Water wants to fall • Potential energy Head Elevation Elevation Head (increases with height above datum) Elevation datum Total Head • For our purposes: • Total head = Pressure head + Elevation head • Water flows down a total head gradient Elevation datum Head Total Head (constant: hydrostatic equilibrium) Elevation P = 0 (= Patm) Potential/Potential Diagrams • Total potential = elevation potential + pressure potential • Pressure potential depends on depth below a free surface • Elevation potential depends on height relative to a reference (slope is 1) Head Gradient • Change in head divided by distance in porous medium over which head change occurs • dh/dx [unitless] Discharge • Q (volume per time) Specific Discharge/Flux/Darcy Velocity • q (volume per time per unit area) • L3 T-1 L-2 → L T-1 Darcy’s Law • Q = -K dh/dx A where K is the hydraulic conductivity and A is the cross-sectional flow area 1803 - 1858 www.ngwa.org/ ngwef/darcy.html Darcy’s Law • Q = K dh/dl A • Specific discharge or Darcy ‘velocity’: qx = -Kx ∂h/∂x … q = -K grad h • Mean pore water velocity: v = q/ne Intrinsic Permeability rw g K k L T-1 L2 Kozeny-Carman Equation 3 2 m n d k 2 1 n 180 Transmissivity • T = Kb Darcy’s Law • Q = -K dh/dl A • Q, q • K, T Mass Balance/Conservation Equation I P O L A • • • • • I = inputs P = production O = outputs L = losses A = accumulation Derivation of 1-D Laplace Equation qx|x • • • • Dz Inflows - Outflows = 0 (q|x - q|x+Dx)DyDz = 0 q|x – (q|x +Dx dq/dx) = 0 dq/dx = 0 (Continuity Equation) h q K x (Constitutive equation) h d K x 0 dx qx|x+Dx Dx Dy h 0 2 x 2 General Analytical Solution of 1-D Laplace Equation h 0 2 x 2 h x 2 x 0x 2 h A x h x A x x h Ax B Particular Analytical Solution of 1-D Laplace Equation (BVP) BCs: - Derivative (constant flux): e.g., dh/dx|0 = 0.01 - Constant head: e.g., h|100 = 10 m After 1st integration of Laplace Equation we have: h A x Incorporate derivative, gives A. After 2nd integration of Laplace Equation we have: h Ax B Incorporate constant head, gives B. Finite Difference Solution of 1-D Laplace Equation h/x|x+Dx/2 h|x x h|x+Dx Estimate here x +Dx Need finite difference approximation for 2nd order derivative. Start with 1st order. h x Dx h x h x Dx h x h x x Dx / 2 x Dx x Dx Look the other direction and estimate at x – Dx/2: h x x Dx / 2 h x h x Dx x x Dx h x h x Dx Dx Finite Difference Solution of 1-D Laplace Equation (ctd) h|x-Dx h/x|x-Dx/2 x -Dx Estimate here h|x h/x|x+Dx/2 x Estimate here h|x+Dx x +Dx 2h/x2|x Estimate here Combine 1st order derivative approximations to get 2nd order derivative approximation. h 2 x 2 h x x Dx / 2 Dx h x h x Dx h x x Dx / 2 Set equal to zero and solve for h: Dx h x h x Dx Dx Dx hx h x Dx 2h x h x Dx Dx 2 h x Dx h x Dx 2 2-D Finite Difference Approximation y +Dy h|x-Dx,y x -Dx h|x,y+Dy h|x,y h|x+Dx,y x, y x +Dx h|x,y-Dy h x, y h x Dx , y h x Dx , y h x , y Dy h x , y Dy 4 Matrix Notation/Solutions 4h2,2 h2,3 h1,2 h2,1 h3,2 h2,2 4h2,3 h1,3 h2,4 h3,3 4 1 h2, 2 h1, 2 h2,1 h3, 2 1 4 h h h h 2,3 1,3 2, 4 3,3 • Ax=b • A-1b=x Toth Problems • Governing Equation h h 2 0 2 x y • Boundary Conditions 19 17 15 13 11 9 7 5 3 2 1 2 S1 S2 S3 S4 S5 S6 S7 S8 S9 S10 S11 10.09-10.1 10.08-10.09 10.07-10.08 10.06-10.07 10.05-10.06 10.04-10.05 10.03-10.04 10.02-10.03 10.01-10.02 10-10.01 Recognizing Boundary Conditions S1 • Parallel: S3 S5 – Constant Head – Constant (non-zero) Flux S7 S9 S11 • Perpendicular: No flow • Other: S13 S15 S17 S19 – Sloping constant head S21 S23 S25 S29 13 10 7 4 1 S27 Internal ‘Boundary’ Conditions • No flow S11 S3 S5 S7 S9 S11 S13 S15 S17 S19 S21 S23 S25 S27 S29 4 7 10 – Wells – Streams – Lakes 13 • Constant head S1 S3 S5 – Flow barriers S7 S9 • Other S11 S13 S15 S17 S19 15 13 11 9 7 5 3 1 S21 S23 Poisson Equation R • Add/remove water from system so that q | inflow and outflow are different • R can be recharge, ET, well pumping, etc. • R can be a function of space and time • Units of R: L T-1 xx qx|x+Dx b Dx Dy Poisson Equation R (qx|x+Dx - qx|x)Dyb -RDxDy = 0 h q K x h K x x Dx h x qx|x qx|x+Dx b Dx Dy h K Dyb RDxDy x x h x R x Dx x Dx T 2h R 2 x T Dupuit Assumption • Flow is horizontal • Gradient = slope of water table • Equipotentials are vertical Dupuit Assumption (qx|x+Dx hx|x+Dx- qx|x hx|x)Dy - RDxDy = 0 h q K x h h hx Dx K hx Dy RDxDy K x x x x Dx h h 2h x x 2 h 2 x h 2 x R x Dx x 2Dx K h 2R 2 x K 2 2 Capture Zones Water Balance and Model Types Water Balance h 0 y x ,1000 • Given: – Recharge rate – Transmissivity h 0 x 1000, y h 0 x 0, y • Find and compare: – Inflow – Outflow h x ,0 0 Water Balance • Given: – Recharge rate – Flux BC – Transmissivity • Find and compare: – Inflow – Outflow Block-centered model Effective outflow boundary 2Dy Y Only the area inside the boundary (i.e. [(imax -1)Dx] [(jmax -1)Dy] in general) contributes water to what is measured at the effective outflow boundary. 1Dy 0 0 1Dx X 2Dx In our case this was 23000 11000, as we observed. For large imax and jmax, subtracting 1 makes little difference. Mesh-centered model Effective outflow boundary 2Dy An alternative is to use a mesh-centered model. Y This will require an extra row and column of nodes and the constant heads will not be exactly on the boundary. 1Dy 0 0 1Dx X 2Dx Dupuit Assumption Water Balance Effective outflow area h1 (h1 + h2)/2 h2 Geostatistics Basic definitions • Variance: n 1 2 var( K ) Ki K mean n 1 var( K ) 2 • Standard Deviation: var( K ) Basic definitions • Number of pairs Basic definitions • Number of pairs: n ( n 1) n pairs 2 Basic definitions • Lag (h) – Separation distance (and possibly direction) h Basic definitions • Variance: n 1 2 var( K ) Ki K mean n 1 h • Variogram: n(h) 1 2 K (x) K (x h) h 2n ( h ) 1 The variogram • Captures the intuitive notion that samples taken close together are more likely to be similar that sample taken far apart Common Variogram Models Common Variogram Models Basic definitions Kriging: N K x wi Ki 1 N w i 1 1 BLUE Kriging Estimates Random Numbers; Pure Nugget # # One variable definition: # to start the variogram modeling user interface. # data(K): 'rand.csv', x=1, y=2, v=3; Unconditioned Simulation • • • • Specify mean and neighborhood Specify variogram Simulation should honor variogram .cmd file/mask map # Unconditional Gaussian simulation on a mask # (local neighborhoods, simple kriging) # defines empty variable: ncols nrows cellsize xllcorner yllcorner 0 data(dummy): dummy, sk_mean=100, max=20, min=10, force; variogram(dummy): 10 Sph(10); mask: 'gridascii.prn'; method: gs; # Gaussian simulation instead of kriging predictions(dummy): 'gs.out'; 60 40 1 0 0 0 0 ... Unconditional Simulation Simulated Field/Known Variogram Conditional Gaussian Simulation • Specify data • Fit and specify variogram • Simulation should honor variogram and be responsive to values at ‘conditioning’ points # Gaussian simulation, conditional upon data # (local neighborhoods, simple kriging) data(SC): 'SC_rand.csv', x=1, y=2, v=3,average,max=20, sk_mean=1400; method: gs; variogram(SC): 400000Nug(0)+3.5e+006 Gau(0.035); #Gridded Output mask: 'ga_SC.prn'; predictions(SC): 'SC_pred.prn'; Kriging • Specify data • Fit and specify variogram • Simulation should honor variogram and return exact values at sampling points • Optimal estimate too far from sample data is mean # # Kriging # (local neighbourhoods, simple and ordinary kriging) # data(SC): 'SC_rand.csv', x=1, y=2, v=3,average,max=20, sk_mean=1400; variogram(SC): 400000Nug(0)+3.5e+006 Gau(0.035); #Gridded Output mask: 'ga_SC.prn'; predictions(SC): 'SC_Krpred.prn'; Gaussian Simulation/Kriging Kriging 500 400 300 200 100 0 Bin 5000 6000 7000 8000 9000 10000 More 6000 7000 8000 9000 10000 More Histogram 5000 Bin 4000 3000 2000 1000 0 -1000 -2000 -3000 -4000 -5000 0 4000 3000 2000 1000 0 -1000 -2000 -3000 -4000 -5000 Frequency Gaussian Frequency Gaussian Simulation/Kriging Histogram 150 100 50 Transient Ground Water Flow Transient Flow Equation I O A DVw = DxDy S Dh Vw h DxDyS t t (qx|x - qx|x+Dx)Dyb + (qy|y - qy|y+Dy)Dxb = SDxDyh/t h h K x K x x h x h h Dyb K y K y x Dx y x Dx Dx h h x x y y Dy Dy h Dxb SDxDy t y Dy h y y S h T t 2 h 2 h S h x 2 y 2 T t Finite Difference t-Dt h|x, t-Dt x -Dx h/t|t-Dt/2 h Dh hx , y ,t hx , y ,t Dt t Dt Dt x +Dx Estimate here t x h|x, t h x Dx , y ,t Dt 2h x , y ,t Dt h x Dx , y ,t Dt Dx 2 hx , y ,t hx , y ,t Dt h x , y Dy ,t Dt 2h x , y ,t Dt h x , y Dy ,t Dt Dy 2 S hx , y ,t hx , y ,t Dt T Dt TDt h x Dx , y ,t Dt 4h x , y ,t Dt h x Dx , y ,t Dt h x , y Dy ,t Dt h x , y Dy ,t Dt 2 S Dx CFL Condition • The stability criterion (for 1-D) is: T/S Dt/Dx2 ½ Quasi-3D Models Leakance and head-dependent boundaries Assumptions: • Flow is 2-D horizontal in ‘aquifer’ layers • Flow is vertical in ‘confining’ layers • There is a significant difference in hydraulic conductivity between aquifers and confining layers • Aquifer layers are connected by leakage across confining layers Schematic T2 (or K2) b2 (or h2) i=2 k2 d2 T1 b1 k1 d1 i=1 Pumped Aquifer Heads T2 (or K2) b2 (or h2) i=2 k2 d2 T1 b1 k1 d1 i=1 Heads h2 h2 - h1 T2 (or K2) b2 (or h2) i=2 h1 k2 d2 T1 b1 k1 d1 i=1 Flows h2 h2 - h1 h1 T2 (or K2) b2 (or h2) i=2 qv k2 d2 T1 b1 k1 d1 i=1 Leakance Leakage coefficient, resistance (inverse) • Leakance k d • From below: ki 1 qv hi 1 hi d i 1 • From above: ki 1 qv hi 1 hi d i 1 Equations • Fully 3-D h h h Kx K y Kz 0 x x y y z z • Confined hi hi ki 1 ki 1 T T h h h h Ri 0 xi yi i 1 i i 1 i x x y y d i 1 d i 1 • Unconfined hi hi ki 1 K xi hi K yi hi hi 1 hi Ri 0 x x y y d i 1 Poisson Equation h R qv 2 x T 2 R qv h x Dx h x Dx Dx T 2 2 h x, y Finite Elements f: basis functions Finite Elements f: hat functions Fracture/Conduit Flow Basic Fluid Dynamics Momentum • p = mu Viscosity • • • • Resistance to flow; momentum diffusion Low viscosity: Air High viscosity: Honey Kinematic viscosity: r Reynolds Number • The Reynolds Number (Re) is a non-dimensional number that reflects the balance between viscous and inertial forces and hence relates to flow instability (i.e., the onset of turbulence) • Re = v L/ • L is a characteristic length in the system • Dominance of viscous force leads to laminar flow (low velocity, high viscosity, confined fluid) • Dominance of inertial force leads to turbulent flow (high velocity, low viscosity, unconfined fluid) Re << 1 (Stokes Flow) Tritton, D.J. Physical Fluid Dynamics, 2nd Ed. Oxford University Press, Oxford. 519 pp. Separation Eddies, Cylinder Wakes, Vortex Streets Re = 30 Re = 40 Re = 47 Re = 55 Re = 67 Re = 100 Re = 41 Tritton, D.J. Physical Fluid Dynamics, 2nd Ed. Oxford University Press, Oxford. 519 pp. Poiseuille Flow y z u x a L Flow Poiseuille Flow • In a slit or pipe, the velocities at the walls are 0 (no-slip boundaries) and the velocity reaches its maximum in the middle • The velocity profile in a slit is parabolic and given by: 2 G a 2 ux x 2 2 • G can be due to gravitational acceleration (G = rg in a vertical slit) or the linear pressure gradient (Pin – Pout)/L u(x) x=0 x = a/2 Poiseuille Flow 2 G a 2 ux x 2 2 • Maximum umax G a 2 2 2 u(x) • Average 2 G 2 uaverage umax a 3 12 x=0 x = a/2 Kirchoff’s Current Law • Kirchoff’s law states that the total current flowing into a junction is equal to the total current leaving the junction. I1 Gustav Kirchoff was an 18th century German mathematician I1 flows into the node I2 flows out of the node I3 flows out of the node node I2 I1 = I2 + I3 I3 • Ohm’s law relates the flow of current to the electrical resistance and the voltage drop • V = IR (or I = V/R) where: – I = Current – V = Voltage drop – R = Resistance • Ohm’s Law is analogous to Darcy’s law • Poiseuille's law can related to Darcy’s law and subsequently to Ohm's law for electrical circuits. uave 1 DP 2 a 12 L Q uave A 1 DP 2 Q aa 12 L A = a *unit depth • Cubic law: a DP Q 12 L 3 Q Ki 3 a K 12 36 lu Fracture Network DP12 Q12 DP DP12 DP23 DP34 DP45 DP56 L12 Q23 L 23 DP DP23 Q34 DP34 L45 Q45 DP45 Q56 DP56 -216 lu - Q12 Q34 Q56 Q23 Q45 Q12 2Q23 Matrix Form DP23 DP12 K12 2 K 23 0 L L DP23 DP34 2 K 23 K 34 0 L L DP34 DP45 K 34 2 K 45 0 L L DP45 DP56 2 K 45 K 56 0 L L K12 0 0 0 L12 2 K 23 2 K 23 0 0 L23 DP DP12 DP23 DP34 DP45 DP56 0 K 34 K 34 0 L34 0 0 2 K 45 2 K 45 L45 DP12 L 12 0 DP23 0 0 L23 0 DP 0 34 0 L34 K56 DP 0 45 L56 L DP DP45 56 L56 Back Solution • Have conductivities and, from the matrix solution, the gradients DP12 – Compute flows Q K12 L • Also have end pressures – Compute intermediate pressures from DPs Hydrologic-Electric Analogy Poiseuille's law corresponds to the Kirchoff/Ohm’s Law for electrical circuits, where pressure drop Δp is replaced by voltage V and flow rate by current I DaP DP12 DP23 DP34 DP45 DP56 Vmax I12 ΔP12 I23 DP a 2 2 rL 2 R I34 ΔP34 I45 I45 I56 ΔP56 V R I23 ΔP23 ΔP45 I Q = 0.11 lu3/ts Q = 0.11 lu3/ts Kirchoff LBM Re 0.66 1.0 1.8 4.1 7.2 43.0 1 K Q (lu3/ts) LBM Kirchoff’s 0.11 0.11 0.14 0.14 0.18 0.19 0.27 0.28 0.36 0.37 0.87 0.92 Eddies Serpa, CY, 2005, Unpublished MS Thesis, FIU Bai, T., and Gross, M.R., 1999, J Geophysical Res, 104, 1163-1177 Flow 3 mm 3.3 mm x 2.7 mm Re = 9 Non-curving cross joint 4.0E-03 Non-linear y = 0.29x + 0.00 R2 = 1.00 3.5E-03 2.5E-03 2.0E-03 1.5E-03 1.0E-03 5.0E-04 0.0E+00 0.0E+00 2.0E-03 4.0E-03 6.0E-03 8.0E-03 1.0E-02 1.2E-02 1.4E-02 HEAD GRADIENT Non-curving cross joint Poiseuille Law Non-linear 0.295 0.290 HYDRAULIC CONDUCTIVITY (m/s) FLUX (m/s) 3.0E-03 0.285 0.280 0.275 0.270 0.265 0.260 0.255 0.250 0.1 1.0 10.0 REYNOLDS NUMBER 100.0