An Efficient Multicomponent Numerical Simulator

1978 ◽  
Vol 18 (05) ◽  
pp. 355-368 ◽  
Author(s):  
H. Kazemi ◽  
C.R. Vestal ◽  
Deane G. Shank

Original manuscript received in Society of Petroleum Engineers office Sept. 15, 1977. Paper accepted for publication April 21, 1978. Revised manuscript received July 27. 1978. Paper (SPE 6890) first presented at the SPE-AIME 52nd Annual Fall Technical Conference and Exhibition, held in Denver, Oct. 9-12, 1977. Abstract An efficient, three-dimensional three-phase, multicomponent, numerical reservoir simulator was developed to study petroleum reservoirs where interphase mass transfer is important. Flow equations have a volume balance on the water phase and a mole balance on the vapor-liquid hydrocarbon phases. Additional equations include the capillary phases. Additional equations include the capillary pressure, phase equilibrium, and saturation pressure, phase equilibrium, and saturation relations. Flow equations, in finite-difference form, are combined to obtain an implicit equation for the oil-phase pressure, an explicit equation for the over-all composition of each hydrocarbon component, an explicit water saturation equation, and explicit oil-gas saturation equations that satisfy thermo-dynamic equilibrium. Equations for oil pressure, water saturation, hydrocarbon compositions, and oil-gas saturations are sequentially solved in an iterative loop until convergence is achieved. The simplicity of the sequential solution algorithm presented here is believed to be a new contribution. Furthermore, if thermodynamic inconsistencies appear in the entry data, these can be detected readily from the pressure and other equations in the sequential pressure and other equations in the sequential algorithm. Introduction With deeper drilling, more reservoirs containing volatile crude oils and gas condensates have been found. To study the performance of such reservoirs and to assist in maximizing hydrocarbon recovery, compositional reservoir simulators are needed. These simulators account for multiphase flow and the interphase mass transfer of each component in the given hydrocarbon system. This simply means that at any given time the simulator tracks the motion of reservoir fluids and calculates the state of equilibrium at many strategic reservoir points (simulator nodes). Therefore, at each reservoir points the phase pressures, the phase saturations, the over-all composition, the mole fraction of each component in the liquid and in the vapor phase, and the liquid mole fraction are calculated with time. Several tank material-balance methods provided the early computational approach to reservoir performance predictions. The experience gained performance predictions. The experience gained in the formulation and in the use of the tank models became the foundation of our knowledge for developing the multidimensional compositional simulator of this paper. Four papers, using finite-difference computational schemes, were instrumental in helping us make the transition from the tank model to the multidimensional case. This paper provides formulation for a multicomponent numerical reservoir simulator. We have tried to provide the formulation with enough detail so that the reader can use it as an easily accessible starting point for his own research and development. This formulation is efficient in the sense that it is computationally less expensive than fully implicit schemes and can be used effectively for a wide range of practical problems. Quantitatively, for an N-component, three-phase (water, oil, and gas) system, 3N + 7 variables (Pw, Po, Pg, Sw, Sg, and xi, yi, zi, i = 1,2,....., N, Po, Pg, Sw, Sg, and xi, yi, zi, i = 1,2,....., N, and L) are usually determined at each reservoir node at any given time. For comparison, in a black-oil simulator, six variables (Pw, Po, Pg, Sw, So, and Sg) are calculated at each node. This comparison points out that a compositional reservoir simulator requires more bookkeeping and more storage. After we have described the details of the computation in later sections, it will be recognized that the computation time can be several-fold, too. However, an efficient mathematical scheme, such as the one presented here, brings the computation time close to that of a black-oil simulator. Flow equations have a volumetric balance on the water phase and a molar balance on the hydrocarbon phases. Hydrocarbon-phase equilibrium calculations phases. Hydrocarbon-phase equilibrium calculations use equilibrium ratios as a function of pressure and convergence pressure. Densities and viscosities are calculated in the most general case as functions of pressure and composition of the given phase. Flow equations are discretized in an implicit finite-difference form to obtain an implicit pressure equation, an explicit water-saturation equation, an explicit composition equation, and two explicit gas-oil saturation equations. SPEJ P. 355

Author(s):  
A. M. Abdel Dayem

Quasi-1D Euler equations have a considerable part of research to allow the prediction of the internal and external flows of the aerodynamic applications. Numerical solving of these equations by a so-called computational fluid dynamics (CFD) finds a very close agreement of the flow solver regarding to the experimental tests. Using CFD in the aerodynamic design is a new area of research that can be a useful addition in this field. Aerodynamic design of a subsonic and transonic converged-diverged nozzle is the task of this work. ARC1D is a robust algorithm used in the aerodynamic numerical simulation area. Developing ARC1D code and an objective function that is constrained by the nozzle axial velocity are considered. The nozzle design is optimized with various numbers of design variables (nozzle cross-sectional area) versus the accuracy and computation time. The discretized flow equations of Quasi-1D Euler equations, finite-difference scheme and optimality conditions are simultaneously solved in a single system of nonlinear equations. KSOPT optimization algorithm was efficiently used in the problem optimization without design constraints. It can be concluded that the code obtained good results regardless the computation time that is not a critical factor in the one-dimensional solution. Also, the finite-difference of the gradient of the objective function was found efficient in the design optimization with accepted computation time.


1970 ◽  
Vol 10 (03) ◽  
pp. 257-267 ◽  
Author(s):  
A. Spivak ◽  
K.H. Coats

Abstract This paper describes the use of a multiphase, multidimensional mathematical model to predict two- and three-phase coning behavior. Severe computational instability in the form of saturation oscillations in grid blocks near the wellbore is commonly encountered in the mathematical simulation of coning. This instability is due to the explicit (dated at the beginning of a time step and held constant for that time step) handling of saturation - dependent transmissibilities and production terms in the finite-difference solution of production terms in the finite-difference solution of the flow equations. An analysis of stability with respect to explicit handling of saturation-dependent transmissibilities is presented in this paper. This analysis shows why explicit transmissibilities can result in a severe time-step restriction for coning simulation. The use of implicit production terms in the difference equations to reduce instabilities is discussed and examples are given. These examples show that the implicit handling of production terms alone can result in a fivefold increase and permissible time step for a coning simulation with virtually no increase in computing time per time step. A laboratory water-coning experiment was simulated and excellent agreement was obtained between computed and observed results. A three-phase coning example for a gravity-segregation reservoir is also presented. Introduction Simulation of coning behavior is normally done by numerically solving the flow equations expressed in cylindrical (r, z, theta) coordinates with symmetry in the theta direction. The finite-difference technique of numerical solution of differential equations requires that the portion of the reservoir being simulated be divided into grid blocks as shown in Fig. 1. Since coning is a well phenomenon and not a gross reservoir phenomenon, the grid blocks must necessarily be relatively small in the vicinity of the wellbore because both pressures and saturations vary rapidly in this region. Severe computational instability is commonly encountered in the simulation of coning due to the relatively small grid-block sizes and high flow velocities in the vicinity of the wellbore. During a time step that would be considered normal for most reservoir simulation problems, a block near the wellbore is required to pass a volume of fluid many times its pore volume. SPEJ P. 257


2016 ◽  
Vol 873 ◽  
pp. 18-22
Author(s):  
Ming Li Huang ◽  
Xue Shen ◽  
Hong Xiao Li

The equilibrium alloys closed to Mg-Nd side in the Mg-rich corner of the Mg-Zn-Nd system at 400°C have been investigated by scanning electron microscopy, electron probe microanalysis and X-ray diffraction. The binary solid solutions Mg12Nd and Mg3Nd with the solubility of Zn have been identified. The maximum solubility of Zn in Mg12Nd is 4.8at%, and Mg12Nd phase can be in equilibrium with Mg solid solution. However, only when the solubility range of Zn in 26at%~32.2at%, Mg3Nd can be in two-phase equilibrium with Mg solid solution. As the results, two two-phase regions as Mg+Mg12Nd and Mg+Mg3Nd and a three-phase region as Mg+Mg12Nd+Mg3Nd in Mg-Nd-Zn ternary isothermal section at 400°C have been identified.


2007 ◽  
Author(s):  
Abbas Firoozabadi ◽  
Kjetil Braathen Haugen ◽  
Lixin Sun

2015 ◽  
Vol 3 (1) ◽  
pp. SA159-SA166 ◽  
Author(s):  
Larry Jacobson ◽  
Venkataraman Jambunathan ◽  
Zhipeng Liu ◽  
Weijun Guo

Recently developed multidetector pulsed-neutron tools (MDPNTs — a term describing a pulsed-neutron tool with at least three detectors) can provide three-phase formation fluid analysis in cased wells. These tools are 43 mm (1 11/16 in.) or 54 mm (2 1/8 in.) in diameter and can be logged in or below most tubing sizes. We reviewed traditional oil- and water-saturation techniques as well as indirect gas-saturation techniques, and we compared them with recently developed direct gas-saturation techniques, now available from MDPNTs. A log example developed the data verification and interpretation process. The interpretation process was divided into two parts: First, we verified the log data quality and second, we applied a newly developed gas model to the log data providing gas saturation without any reliance on the previously determined oil and water saturation.


Geophysics ◽  
1995 ◽  
Vol 60 (5) ◽  
pp. 1514-1526 ◽  
Author(s):  
Richard T. Coates ◽  
Michael Schoenberg

For the purposes of seismic propagation, a slip fault may be regarded as a surface across which the displacement caused by a seismic wave is discontinuous while the stress traction remains continuous. The simplest assumption is that this slip and the stress traction are linearly related. Such a linear slip interface condition is easily modeled when the fault is parallel to the finite‐difference grid, but is more difficult to do for arbitrary nonplanar fault surfaces. To handle such situations we introduce equivalent medium theory to model material behavior in the cells of the finite‐ difference grid intersected by the fault. Virtually identical results were obtained from modeling the fault by (1) an explicit slip interface condition (fault parallel to the grid) and (2) using the equivalent medium theory when the finite‐difference grid was rotated relative to the fault and receiver array. No additional computation time is needed except for the preprocessing required to find the relevant cells and their associated moduli. The formulation is sufficiently general to include faults in and between arbitrary anisotropic materials with slip properties that vary as a function of position.


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