Computational Fluid Dynamics in Biomedical Systems. A Simple Introduction Boyd Gatlin

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1 Computational Fluid Dynamics in Biomedical Systems A Simple Introduction Boyd Gatlin

2 What I Hope To Do Today Define some common terms Identify some applications of CFD in biology and medicine Describe the steps and processes of CFD Outline a physically intuitive development of sets of CFD equations Present a typical case in medical biology

3 Examples of Biomedical CFD Applications Heart pumping Vessel graft evaluation Blood flow Air flow in lungs Joint lubrication Cell-fluid interface Tendon-sheath Gas exchange Artificial organ design Vocal tract analysis Microbe locomotion Perfusion in tissues Life support systems Nose and sinus flows Spinal fluid flow Cardiac valve design

4 What is a fluid? A fluid is any substance which deforms continuously under a shearing stress Includes liquids and gasses Classified as Newtonian or non-newtonian Water and most gasses are Newtonian Whole blood, synovia, mucus, ketchup, toothpaste, etc., are not

5 What are some fluid properties? Mass density if this remains constant in a flow, the fluid is incompressible Viscosity a measure ρ of resistance to flow varies with temperature for Newtonian fluids varies with local flow conditions (strain and shear) for non-newtonian

6 What are some properties of the flow itself? Laminar, transitional, or turbulent Compressible or incompressible Confined (contained in a conduit), partially confined (open channel), or unconfined (flow over an object in the open) Subsonic, supersonic, hypersonic Reacting or non-reacting Single-phase or multi-phase

7 What is CFD? Computational Fluid Dynamics is a set of procedures, carried out in sequence or in parallel, by which the classical equations of fluid motion, plus any auxiliary relations, are approximated by large sets of algebraic equations which are then solve numerically on computers.

8 How does CFD differ from numerical modeling? CFD is simply the process of obtaining numerical solutions to accepted classical equations (Navier-Stokes, ca 1827) Numerical modeling usually involves the development of equations of assumed form and containing free constants derived from experimental data

9 CFD is the application of first principles of fluid physics Modeling is required within CFD to: Compute fluid properties from empirical relationships Represent the effects of turbulence on the flow Include phenomena which cannot reasonably be computed directly from first principles Account for chemical reactions and phase changes Both computational simulation and modeling involve the numerical solution of very large sets of equations on computers

10 CFD by the Numbers I. State the Problem II. Identify Physics & Chemistry III. Identify the Geometry Domain IV. Formulate the Mathematical Statement V. Discretize Equations & Geometry VI. Develop or Choose the Algorithm

11 CFD by the Numbers VII. Develop or Select Software VIII.Choose Computing Hardware IX. Compute the Solution X. Analyze & Interpret Results A. Storage and Manipulate Large Data Sets B. Post Processing and Visualization

12 Statement of Problem Clearly identified (What is the shearing stress on an artery graft during systole?) Separated from irrelevant, extraneous or non-essential issues Constrained so that key parameters and variables can be isolated so much as possible

13 Identification of Physics Physical principles related to the problem Statement of physical principles in mathematical form Reduction of complexity to make amenable to computation Identification of auxiliary relations (turbulence model, non-newtonian effects, property variations, etc.)

14 Problem Geometry Set the physical boundaries; define the domain Obtain data by measurement, digitized scans, etc. Observe boundary conditions of physics Generate bounding surfaces (sets of cross sections, algebraic models, etc.)

15 Mathematical Statement Generally, Navier-Stokes equations, or some subset Equation of state (e.g., ideal gas law) Relationship between fluid and surfaces, and between different fluids (mucus, porosity) Appropriate boundary and initial conditions Turbulence model Fluid property models and reaction equations

16 Discretization Divide the problem domain into a very large number of very small regions using a grid Replace the classical differential equations with sets of finite difference or finite volume equations Balance accuracy needs with computing capacity (3-D is very much bigger than 2-D)

17 A grid (mesh) is a system of uniquely identifiable and indexed points in space upon who continuous functions may be approximated through some method of discretization. Structured Unstructured Orthogonal Uniform Boundary fitted Rectilinear Fine Non-orthogonal Non-uniform Non-boundary fitted Non-rectilinear Coarse

18 Typical CFD Grids Structured Unstructured

19 Grids Before Descartes

20 Discretization of Mathematics Finite difference approximation---replace derivatives with ratios of differences at each grid point Mathematically intuitive Physics less obvious Finite volume formulation---apply physical conservation laws to each small volume formed by grid lines Mathematically simple, if not naïve Physically intuitive Finite element methods---a family of techniques that are generally not physically intuitive

21

22 Discretization of Mathematics Finite difference approximation---replace derivatives with ratios of differences at each grid point Mathematically intuitive Physics less obvious Finite volume formulation---apply physical conservation laws to each small volume formed by grid lines Mathematically simple, if not naïve Physically intuitive Finite element methods---a family of techniques that are generally not physically intuitive

23 Simple Finite Difference Approximation of a Derivative u u u( i + 1) u() i ; ; x x x( i + 1) x() i

24 Finite Control Volume Mass, energy,momentum inflow/outflow Mass, energy, momentum stored Net mass, energy and momentum entering the volume is forced to balance that leaving and that stored in the FV

25 Algorithm Method by which the large system of equations will be solved Choose based on mathematical character, method of discretization; there is no one size fits all available Poor choices, based on available hardware & software, may lead to failure

26 Software Software translates algorithm statements into computer operations Ample CFD software available, much unsuited for biomedical applications Poor choices may lead to complete failure of the computational simulation

27 Computing Hardware PC vs workstation vs supercomputer Serial vs parallel platform Considerations Physical size of problem (number of grid points) Whether problem is steady or unsteady Time scales involved Availability

28 Solution Goal is to obtain solution to the problem not just to the mathematical statement Expect false starts, adjustment of boundary & initial conditions Monitor intermediate results for reasonableness Validate solution method on problem for which solution is known

29 Analysis & Interpretation Post process solution data Calculate derivative variables (pressure gradients, shear stresses, etc.) Compare with data or similar solutions Use visualization tools Examine distributions, look for trends Animate in time or space

30 Respiratory Flow in A Bifurcation: A Case Study

31 Problem Statement Flow development in airways of the lung is not understood well enough by medical science and cannot be satisfactorily measured.

32 Mathematical Model Air flow at low speeds is well predicted by the incompressible form of the Navier- Stokes Equations Air at low speeds is a constant-property, Newtonian fluid Flow is mostly laminar in small airways Rigid walls are a valid first approximation

33

34 Geometric Domain Airway tree is hopelessly complex Branching pattern is not reproducible

35 Surfaces of Selected Model

36 Discretization of Geometry Structured, finite-volume grid

37 Discretizaton & Algorithm Finite volume formulation (enforce conservation laws) Implicit time stepping (solution is computed at new time level) Inherently stable because closer to physics Larger time steps possible Newton iteration to converge each time step

38 Visualization of Results

39

40 Animation of Simulation of Flow in an Asymmetric Bifurcation Lung airways do not branch symmetrically Effects of axial curvature important Real flow does not enter smoothly Inlet & outlet conditions unknown

41 Oscillatory Flow in a Lung-Like Bifurcation Colors represent fluid speed Skewness due to friction and curvature Details not available from experiment Colored profiles act like porous membranes which stretch in proportion to the local fluid speed.

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