Predicting Flow Reversals in a Computational Fluid Dynamics Simulated Thermosyphon using Data Assimilation

Predicting Flow Reversals in a Computational Fluid Dynamics Simulated Thermosyphon using Data Assimilation

Andrew J. Reagan
Abstract

A thermal convection loop is a circular chamber filled with water, heated on the bottom half and cooled on the top half. With sufficiently large forcing of heat, the direction of fluid flow in the loop oscillates chaotically, forming an analog to the Earth’s weather. As is the case for state-of-the-art weather models, we only observe the statistics over a small region of state space, making prediction difficult. To overcome this challenge, data assimilation methods, and specifically ensemble methods, use the computational model itself to estimate the uncertainty of the model to optimally combine these observations into an initial condition for predicting the future state. First, we build and verify four distinct DA methods. Then, a computational fluid dynamics simulation of the loop and a reduced order model are both used by these DA methods to predict flow reversals. The results contribute to a testbed for algorithm development.

Predicting Flow Reversals in a Computational Fluid Dynamics Simulated Thermosyphon using Data Assimilation

A Thesis Presented

by

Andrew J. Reagan

to

The Faculty of the Graduate College

of

The University of Vermont

In Partial Fullfillment of the Requirements

for the Degree of Master of Science

Specializing in Applied Mathematics

January, 2014

Accepted by the Faculty of the Graduate College, The University of Vermont, in partial fulfillment of the requirements for the degree of Master of Science, specializing in Applied Mathematics.


Thesis Examination Committee:

Advisor
Christopher M. Danforth, Ph.D.
Peter Sheridan Dodds, Ph.D.
Chairperson
Darren Hitt, Ph.D.

Dean, Graduate College
Cynthia J. Forehand, Ph.D.
Date: November 15, 2013

in dedication to

my parents, Donna and Kevin Reagan, for their unwavering support.

Acknowledgements

I would like to thank Professors Chris Danforth and Peter Dodds for their outstanding advising, as well as Professors Darren Hitt and Yves Dubief for their valuable feedback. This work was made possible by funding from the Mathematics and Climate Research Network and Vermont NASA EPSCoR program. I would like to thank my fellow students for all of their help and toleration through the past two years. And finally I would like to thank my girlfriend Sam Spisiak, whose love makes this thesis worth writing.

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Chapter 1 Introduction

In this chapter we explore the current state of numerical weather prediction, in particular data assimilation, along with an introduction to computational fluid dynamics and reduced order experiments.

1.1 Introduction

Prediction of the future state of complex systems is integral to the functioning of our society. Some of these systems include weather [Hsiang et al. 2013], health [Ginsberg et al. 2008], the economy [Sornette and Zhou 2006], marketing [Asur and Huberman 2010] and engineering [Savely et al. 1972]. For weather in particular, this prediction is made using supercomputers across the world in the form of numerical weather model integrations taking our current best guess of the weather into the future. The accuracy of these predictions depend on the accuracy of the models themselves, and the quality of our knowledge of the current state of the atmosphere.

Model accuracy has improved with better meteorological understanding of weather processes and advances in computing technology. To solve the initial value problem, techniques developed over the past 50 years are now broadly known as data assimilation. Formally, data assimilation is the process of using all available information, including short-range model forecasts and physical observations, to estimate the current state of a system as accurately as possible [Yang et al. 2006].

We employ a toy climate experiment as a testbed for improving numerical weather prediction algorithms, focusing specifically on data assimilation methods. This approach is akin to the historical development of current methodologies, and provides a tractable system for rigorous analysis. The experiment is a thermal convection loop, which by design simplifies our problem into the prediction of convection. The dynamics of thermal convection loops have been explored under both periodic [Keller 1966] and chaotic [Welander 1995, Creveling et al. 1975, Gorman and Widmann 1984, Gorman et al. 1986, Ehrhard and Müller 1990, Yuen and Bau 1999, Jiang and Shoji 2003, Burroughs et al. 2005, Desrayaud et al. 2006, Yang et al. 2006, Ridouane et al. 2010] regimes. A full characterization of the computational behaivor of a loop under flux boundary conditions by Louisos et. al. describes four regimes: chaotic convection with reversals, high Ra aperiodic stable convection, steady stable convection, and conduction/quasi-conduction [Louisos et al. 2013]. For the remainder of this work, we focus on the chaotic flow regime.

Computational simulations of the thermal convection loop are performed with the open-source finite volume C++ library OpenFOAM [Jasak et al. 2007]. The open-source nature of this software enables its integration with the data assimilation framework that this work provides.

1.2 History of NWP

The importance of Vilhelm Bjerknes in early developments in NWP is described by Thompson’s “Charney and the revival of NWP” [Thompson 1990]:

It was not until 1904 that Vilhelm Bjerknes - in a remarkable manifesto and testament of deterministic faith - stated the central problem of NWP. This was the first explicit, coherent, recognition that the future state of the atmosphere is, in principle, completely determined by its detailed initial state and known boundary conditions, together with Newton’s equations of motion, the Boyle-Charles-Dalton equation of state, the equation of mass continuity, and the thermodynamic energy equation. Bjerknes went further: he outlined an ambitious, but logical program of observation, graphical analysis of meterological data and graphical solution of the governing equations. He succeeded in persuading the Norwegians to support an expanded network of surface observation stations, founded the famous Bergen School of synoptic and dynamic meteorology, and ushered in the famous polar front theory of cyclone formation. Beyond providing a clear goal and a sound physical approach to dynamical weather prediction, V. Bjerknes instilled his ideas in the minds of his students and their students in Bergen and in Oslo, three of of whom were later to write important chapters in the development of NWP in the US (Rossby, Eliassen, and Fjörtoft).

It then wasn’t until 1922 that Lewis Richardson suggested a practical way to solve these equations. Richardson used a horizontal grid of about 200km, and 4 vertical layers in a computational mesh of Germany and was able to solve this system by hand [Richardson and Chapman 1922]. Using the observations available, he computed the time derivative of pressure in the central box, predicting a change of 146 hPa, whereas in reality there was almost no change. This discrepancy was due mostly to the fact that his initial conditions (ICs) were not balanced, and therefore included fast-moving gravity waves which masked the true climate signal [Kalnay 2003]. Regardless, had the integration had continued, it would have “exploded,” because together his mesh and timestep did not satisfy the Courant-Friedrichs-Lewy (CFL) condition, defined as follows. Solving a partial differential equation using finite differences, the CFL requires the Courant number to be less than one for a convergent solution. The dimensionless Courant number relates the movement of a quantity to the size of the mesh, written for a one-dimensional problem as for the velocity, the timestep, and the mesh size.

Early on, the problem of fast traveling waves from unbalanced IC was solved by filtering the equations of motion based on the quasi-geostrophic (slow time) balance. Although this made running models feasible on the computers available during WW2, the incorporation of the full equations proved necessary for more accurate forecasts.

The shortcomings of our understanding of the subgrid-scale phenomena do impose a limit on our ability to predict the weather, but this is not the upper limit. The upper limit of predictability exists for even a perfect model, as Edward Lorenz showed in with a three variable model found to exhibit sensitive dependence on initial conditions [Lorenz 1963].

Numerical weather prediction has since constantly pushed the boundary of computational power, and required a better understanding of atmospheric processes to make better predictions. In this direction, we make use of advanced computational resources in the context of a simplified atmospheric experiment to improve prediction skill.

1.3 IC determination: data assimilation

Areas as disparate as quadcopter stabilization [Achtelik et al. 2009] to the tracking of ballistic missle re-entry [Siouris et al. 1997] use data assimilation. The purpose of data assimilation in weather prediction is defined by Talagrand as “using all the available information, to determine as accurately as possible the state of the atmospheric (or oceanic) flow.” [Talagrand 1997] One such data assimilation algorithm, the Kalman filter, was originally implemented in the navigation system of Apollo program [Kalman and Bucy 1961, Savely et al. 1972].

Data assimilation algorithms consist of a 3-part cycle: predict, observe, and assimilate. Formally, the data assimilation problem is solved by minimizing the initial condition error in the presence of specific constraints. The prediction step involves making a prediction of the future state of the system, as well as the error of the model, in some capacity. Observing systems come in many flavors: rawindsomes and satellite irradiance for the atmosphere, temperature and velocity reconstruction from sensors in experiments, and sampling the market in finance. Assimilation is the combination of these observations and the predictive model in such a way that minimizes the error of the initial condition state, which we denote the analysis.

The difficulties of this process are multifaceted, and are addressed by parameter adjustments of existing algorithms or new approaches altogether. The first problem is ensuring the analysis respects the core balances of the model. In the atmosphere this is the balance of Coriolis force and pressure gradient (geostrophic balance), and in other systems this can arise in the conservation of physical (or otherwise) quantities.

In real applications, observations are made with irregular spacing in time and often can be made much more frequently than the length of data assimilation cycle. However the incorporation of more observations will not always improve forecasts: in the case where these observations can only be incorporated at the assimilation time, the forecasts can degrade in quality [Kalnay et al. 2007]. Algorithms which are capable of assimilating observations at the time they are made have a distinct advantage in this respect. In addition, the observations are not always direct measurements of the variables of the model. This can create non-linearities in the observation operator, the function that transforms observations in the physical space into model space. In Chapter 2 we will see where a non-linear operator complicates the minimization of the analysis error.

As George Box reminds us, “all models are wrong” [Box et al. 1978]. The incorporation of model bias into the assimilation becomes important with imperfect models, and although this issue is well-studied, it remains a concern [Allgaier et al. 2012].

The final difficulty we need to address is the computational cost of the algorithms. The complexity of models creates issues for both the computation speed and storage requirements, an example of each follows. The direct computation of the model error covariance, integrating a linear tangent model which propagates errors in the model forward in time, amounts to model integrations where is the number of variables in the model. For large systems, e.g. for global forecast models, this is well beyond reach. Storing a covariance matrix at the full rank of model variables is not possible even for a model of the experiment we will address, which has 240,000 model variables. Workarounds for these specific problems include approximating the covariance matrix (e.g. with a static matrix, or updating it using an ensemble of model runs), and reformulating the assimilation problem such that the covariance is only computed in observation space, which is typically orders of magnitude smaller.

1.4 NWP and fluid dynamics: computational models

As early as 1823, the basic equations governing flow of a viscous, heat-conducting fluid were derived from Newton’s law of motion [Navier 1823, Stokes 1846]. These are the Navier-Stokes equations. The equations of geophysical fluid dynamics describe the flow in Earth’s atmosphere, differing from the Navier-Stokes equations by incorporating the Coriolis effect and neglecting the vertical component of advection. In both cases, the principle equations are the momentum equations, continuity equation and energy equation.

As stated, our interest here is not the accuracy of computational fluid dynamic simulations themselves, but rather their incorporation into the prediction problem. For this reason, we limit the depth of exploration of available CFD models.

We chose to perform simulations in the open-source C++ library OpenFOAM. Because the code is open-source, we can modify it as necessary for data assimilation, and of particular importance becomes the discretized grid.

There are two main directions in which we do explore the computational model: meshing and solving. To solve the equations of motion numerically, we first must discretize them in space by creating the computational grid, which we refer to as a mesh. Properly designing and characterizing the mesh is the basis of an accurate solution. Still, without the use of (notoriously unreliable) turbulence models, and without a grid small enough to resolve all of the scales of turbulence, we inevitably fail to capture the effects of sub-grid scale phenomena. In weather models, where grid sizes for global models are in the 1-5km range horizontally, this is a known problem and is an open area of research. In addition to the laminar equations, to account for turbulence, we explore include the model, model, and large eddy simulations (in 3-dimensions only).

Secondly, the choice of solving technique is a source of numerical and algorithmic uncertainty. The schemes which OpenFOAM has available are dissapative and are limited in scope. That is, small perturbations experience damping (such as the analysis perturbations to an ensemble members in ensemble Kalman filters). Without consideration this problem, the ensemble does not adequately sample the uncertainty of the model to obtain an approximation of the model error growth.

We investigate these meshing and solving techniques in greater detail in Chapter 3.

1.5 Toy climate experiments

Mathematical and computational models span from simple to kitchen-sink, depending on the phenomenon of interest. Simple, or “toy”, models and experiments are important to gain theoretical understanding of the key processes at play. An example of such a conceptual model used to study climate is the energy balance model, Figure 1.1.

Figure 1.1: A schematic of the Energy Balance Model (EBM), a conceptual climate model based on the conservation of energy. , represented by the yellow arrow, represents energy coming from the sun absorbed by Earth’s surface (horizontal green bar). The red, dashed arrow represents energy radiating out of Earth’s surface, of which some is reflected back by the atmosphere (horizontal gray line). Since energy is conserved in the EBM, the parameterizations of surface albedo (amount reflected by Earth’s surface), atmospheric absorbivity, and radiation rate determine the long term behaivor of internal energy (temperature). This schematic was provided in a lecture given by Dr. Chris Jones [Jones 2013].

With a simple model, it is possible to capture the key properties of simple concepts (e.g. the greenhouse effect in the above energy balance model). For this reason they have been, and continue to be, employed throughout scientific disciplines. The “kitchen-sink” models, like the Earth System Models (ESMs) used to study climate, incorporate all of the known physical, chemical, and biological processes for the fullest picture of the system. In the ESM case, the simulations represent our computational laboratory.

We study a model that is more complex than the EBM, but is still analytically tractable, known as the Lorenz 1963 system (Lorenz 63 for short). In 1962, Barry Saltzmann attempted to model convection in a Rayleigh-Bérnard cell by reducing the equations of motion into their core processes [Saltzman 1962]. Then in 1963 Edward Lorenz reduced this system ever further to 3 equations, leading to his landmark discovery of deterministic non-periodic flow [Lorenz 1963]. These equations have since been the subject of intense study and have changed the way we view prediction and determinism, remaining the simple system of choice for examining nonlinear behaivor today [Kalnay et al. 2007].

Thermal convection loops are one of the few known experimental implementations of Lorenz’s 1963 system of equations. Put simply, a thermal convection loop is a hula-hoop shaped tube filled with water, heated on the bottom half and cooled on the top half. As a non-mechanical heat pump, thermal convection loops have found applications for heat transfer in solar hot water heaters [Belessiotis and Mathioulakis 2002], cooling systems for computers [Beitelmal and Patel 2002], roads and railways that cross permafrost [Cherry et al. 2006], nuclear power plants [Detman 1968, Beine et al. 1992, Kwant and Boardman 1992], and other industrial applications. Our particular experiment consists of a plastic tube, heated on the bottom by a constant temperature water bath, and cooled on top by room temperature air.

Figure 1.2: The “kitchen-sink” Earth System Model captures as many known processes as computationally feasible. Models of this size are most useful in making global climate predictions and global weather predictions. By incorporating physically tuned parameterizations of subgrid-scale processes, these models are able to make accurate predictions of Earth’s climate and weather. Due to the size and complexity of the model, the physical processes driving the model dynamics are, however, difficult to study. This schematic describes the Community Earth System Model developed by NCAR [Gardiner 2007].

Varying the forcing of temperature applied to the bottom half of the loop, there are three experimentally accessible flow regimes of interest to us: conduction, steady convection, and unsteady convection. The latter regime exhibits the much studied phenomenon of chaos in its changes of rotational direction. This regime is analytically equivalent the Lorenz 1963 system with the canonical parameter values listed in Table A.6. Edward Lorenz discovered and studied chaos most of his life, and is said to have jotted this simple description on a visit to the University of Maryland [Danforth 2009]:

Chaos: When the present determines the future, but the approximate present does not approximately determine the future.

In chapter 3, we present a derivation of Ehrhard-Müller Equations governing the flow in the loop following the work of Kameron Harris (2011). These equations are akin to the Lorenz 63 system, as we shall see, and the experimental implementation is described in more detail in the first section of Chapter 3.

In chapter 4 we present results for the predictive skill tests and summarize the successes of this work and our contributions to the field. We find that below a critical threshold of observations, predictions are useless, where useless forecasts are defined as those with RMSE greater than 70% of climatological variance. The skill of forecasts is also sensitive to the choice of covariance localization, which we discuss in more detail in chapter 4. And finally, we present “foamLab,” a test-bed for DA which links models, DA techniques, and localization in a general framework with the ability to extend these results and test experimental methods for DA within different models.

Chapter 2 Data Assimilation

The goal of this chapter is to introduce and detail the practical implementation of state-of-the-art data assimilation algorithms. We derive the general form for the problem, and then talk about how each filter works. Starting with the simplest examples, we formulate the most advanced 4-dimensional Variational Filter and 4-dimensional Local Ensemble Transform Kalman Filter to implement with a computational fluid dynamics model. For a selection of these algorithms, we illustrate some of their properties with a MATLAB implementation of the Lorenz 1963 three-variable model:

The cannonical choice of and , produce the well known butterfly attractor, is used for all examples here (Figure 2.1).

Figure 2.1: The Lorenz 63 attractor colored by the norm of the analysis increment. Larger numbers represent where forecasts are poor, and the data assimilation algorithm puts more weight on the observation when initializing a new forecast. This figure was bitmapped for inclusion on the arXiv, for a full version visit http://andyreagan.com.

2.1 Basic derivation, OI

We begin by deriving the equations for optimal interpolation (OI) and for the Kalman Filter with one scalar observation. The goal of our derivation is to highlight which statistical information is useful, which is necessary, and what assumptions are generally made in the formulation of more complex algorithms.

Beginning with the one variable , which could represent the horizontal velocity at one grid-point, say we make two independent observations of : and . If the true state of is given by , then the goal is to produce an analysis of which we call , that is our best guess of .

Denote the errors of by respectively, such that

For starters, we assume that we do not know . Next, assume that the errors vary around the truth, such that they are unbiased. This is written as

As of yet, our best guess of would be the average , and for any hope of knowing well we would need many unbiased observations at the same time. This is unrealistic, and to move forward we assume that we know the variance of each . With this knowledge, which we write

(2.1)

Further assume that these errors are uncorrelated

(2.2)

which in the case of observing the atmosphere, is hopeful.

We next attempt a linear fit of these observations to the truth, and equipped with the knowledge of observation variances we can outperform an average of the observations. For , our best guess of , we write this linear fit as

(2.3)

If is to be our best guess, we desire it to unbiased

and to have minimal error variance .

At this point, note all of the assumptions that we have made: independent observations, unbiased instruments, knowledge of error variance, and uncorrelated observation errors. Of these, knowing the error variances (and in multiple dimensions, error covariance matrices) will become our focus, and better approximations of these errors have been largely responsible for recent improvements in forecast skill.

Solving 2.3, by substituting , we have

To minimize with respect to we compute of the above and solve for 0 to obtain

and similarly for .

We can also state the relationship for as a function of by substituting our form for into the second step of 2.3 to obtain:

(2.4)

This last formula says that given accurate statistical knowledge of , the precision of the analysis is the sum of the precision of the measurements.

Figure 2.2: A 1-dimensional example of this data assimilation cycle. First, a forecast is made with mean 0 and variance 1, labeled . An observation denoted is the made with mean 2 and variance 2. From this information and Equation 2.6 we compute the analysis with mean 2/3, noting the greater reliance on the lower variance input .

We can now formulate the simplest data assimilation cycle by using our forecast model to generate a background forecast and setting . We then assimilate the observations by setting and solving for the analysis velocity as

(2.5)

The difference is commonly reffered to as the “innovation” and represents the new knowledge from the observations with respect to the background forecast. The optimal weight is then given by 2.4 as

(2.6)

The analysis error variance and precision are defined as before, and following Kalnay (2003) for convenience we can rewrite this in terms of as:

(2.7)

We now generalize the above description for models of more than one variable to obtain the full equations for OI. This was originally done by Aerology et al (1960), and independently by Gandin (1965). The following notation will be used for the OI and the other multivariate filters. Consider a field of grid points, where there may be variables at each point for pressure, hydrostatic pressure, temperature, and three dimensions of velocity. We combine all the variables into one list of length where is the product of the number of grid points and the number of model variables. This list is ordered by grid point and then by variable (e.g. for a field with just variables pressure and temperature ). Denote the observations as , where the ordering is the same as but the dimension is much smaller (e.g. by a factor of for NWP) and the observations are not strictly at the locations of or even direct measurements of the variables in . In our experiment, temperature measurements are in the model variable , but are understood as the average of the temperature of the grid points surrounding it within some chosen radius. Examples of indirect and spatially heterogeneous observations in NWP are radar reflectivities, Doppler shifts, satellite radiances, and global positioning system atmospheric refractivities [Kalnay 2003].

We can now write the analysis with similar notation as for the scalar case with the addition of the observation operator which transforms model variables into observation space:

(2.8)
(2.9)
(2.10)

Note that is not required to be linear, but here we write as an matrix for a linear transformation.

Again, our goal is to obtain the weight matrix that minimizes the analysis error . In Kalman Filtering, the weight matrix is called the gain matrix . First, we assume that the background and observations are unbiased.

This a reasonable assumption, and if it does not hold true, we can account for this as a part of the analysis cycle [Dee and Da Silva 1998].

Define the forecast error covariances as

(2.11)
(2.12)
(2.13)

Linearize the observation operator

(2.14)

where are the entries of . Since the background is typically assumed to be a reasonably good forecast, it is convenient to write our equations in terms of changes to . The observational increment is thus

(2.15)
(2.16)

To solve for the weight matrix assume that we know and , and that their errors are uncorrelated:

(2.17)

We now use the method of best linear unbiased estimation (BLUE) to derive in the equation , which approximates . Since and the well known BLUE solution to this simple equation, the that minimizes is given by

Now we solve for the analysis error covariance using from above and . This is (with the final bit of sneakiness using ):

Note that in this formulation, we have assumed that (the observation error covariance) accounts for both the instrumental error and the “representativeness” error, a term coined by Andrew Lorenc to describe the fact that the model does not account for subgrid-scale variability [Lorenc 1981]. To summarize, the equations for OI are

(2.18)
(2.19)

As a final note, it is also possible to derive the “precision” of the analysis but in practice it is impractical to compute the inverse of the full matrix , so we omit this derivation. In general is also not possible to solve for for the whole model, and localization of the solution is achieved by considering each grid point and the observations within some set radius of this. For different models, this equates to different assumptions on the correlations of observations, which we do not consider here.

2.2 3D-Var

Simply put, 3D-Var is the variational (cost-function) approach to finding the analysis. It has been shown that 3D-var solves the same statistical problem as OI [Lorenc 1986]. The usefulness of the variational approach comes from the computational efficiency, when solved with an iterative method. This is why the 3D-Var analysis scheme became the most widely used data assimilation technique in operational weather forecasting, only to be succeeded by 4D-Var today.

The formulation of the cost function can be done in a Bayesian framework [Purser 1984] or using maximum likelihood approach (below). First, it is not difficult to see that solving for for where we define as

(2.20)

gives the same solution as obtained through least squares in our scalar assimilation. The formulation of this cost function obtained through the ML approach is simple [Edwards 1984]. Consider the likelihood of true value given an observation with standard deviation :

(2.21)

The most likely value of given two observations is the value which maximizes the joint likelihood (the product of the likelihoods). Since the logarithm is increasing, the most likely value must also maximize the logarithm of the joint likelihood:

(2.22)

and this is equivalent to minimizing the cost function above.

Jumping straight the multi-dimensional analog of this, a result of Andrew Lorenc [Lorenc 1986], we define the multivariate 3D-Var as finding the that minimizes the cost function

(2.23)

The formal minimization of can be obtained by solving for , and the result from Eugenia Kalnay is [Kalnay 2003]:

(2.24)

The principle difference between the Physical Space Analysis Scheme (PSAS) and 3D-Var is that the cost function is solved in observation space, because the formulation is so similar we do not derive it here. If there are less observations than there are model variables, the PSAS is a more efficient method.

Finally we note for 3D-Var that operationally can be estimated with some flow dependence with the National Meteorological Center (NMC) method, i.e.

(2.25)

with on the order of 50 different short range forecasts. Up to this point, we have assumed knowledge of a static model error covariance matrix , or estimated it using the above NMC method. In the following sections, we explore advanced methods that compute or estimate a changing model error covariance as part of the data assimilation cycle.

2.3 Extended Kalman Filter

The Extended Kalman Filter (EKF) is the “gold standard” of data assimilation methods [Kalnay 2003]. It is the Kalman Filter “extended” for application to a nonlinear model. It works by updating our knowledge of error covariance matrix for each assimilation window, using a Tangent Linear Model (TLM), whereas in a traditional Kalman Filter the model itself can update the error covariance. The TLM is precisely the model (written as a matrix) that transforms a perturbation at time to a perturbation at time , analytically equivalent to the Jacobian of the model. Using the notation of Kalnay [Kalnay 2003], this amounts to making a forecast with the nonlinear model , and updating the error covariance matrix with the TLM , and adjoint model

where is the noise covariance matrix (model error). In the experiments with Lorenz 63 presented in this section, since our model is perfect. In NWP, must be approximated, e.g. using statistical moments on the analysis increments [Danforth et al. 2007, Li et al. 2009].

The analysis step is then written as (for the observation operator):

(2.26)
(2.27)

where

is the innovation. The Kalman gain matrix is computed to minimize the analysis error covariance as

where is the observation error covariance.

Since we are making observations of the truth with random normal errors of standard deviation , the observational error covariance matrix is a diagonal matrix with along the diagonal.

The most difficult, and most computationally expensive, part of the EKF is deriving and integrating the TLM. For this reason, the EKF is not used operationally, and later we will turn to statistical approximations of the EKF using ensembles of model forecasts. Next, we go into more detail regarding the TLM.

2.3.1 Coding the TLM

The TLM is the model which advances an initial perturbation at timestep to a final perturbation at timestep . The dynamical system we are interested in, Lorenz ’63, is given as a system of ODE’s:

We integrate this system using a numerical scheme of our choice (in the given examples we use a second-order Runge-Kutta method), to obtain a model discretized in time.

Introducing a small perturbation , we can approximate our model applied to with a Taylor series around :

We can then solve for the linear evolution of the small perturbation as

(2.28)

where is the Jacobian of . We can solve the above system of linear ordinary differential equations using the same numerical scheme as we did for the nonlinear model.

Figure 2.3: An explanation of how and why the best way to obtain a TLM is with a differentiated numerical scheme.

One problem with solving the system of equations given by Equation 2.28 is that the Jacobian matrix of discretized code is not necessarily identical to the discretization of the Jacobian operator for the analytic system. This is a problem because we need to have the TLM of our model , which is the time-space discretization of the solution to . We can apply our numerical method to the to obtain explicitly, and then take the Jacobian of the result. This method is, however, prohibitively costly, since Runge-Kutta methods are implicit. It is therefore desirable to take the derivative of the numerical scheme directly, and apply this differentiated numerical scheme to the system of equations to obtain the TLM. A schematic of this scenario is illustrated in Figure 2.3. To that the derivative of numerical code for implementing the EKF on models larger than 3 dimensions (i.e. global weather models written in Fortan), automatic code differentiation is used [Rall 1981].

To verify our implementation of the TLM, we propagate a small error in the Lorenz 63 system and plot the difference between that error and the TLM predicted error, for each variable (Figure 2.4).

Figure 2.4: The future error predicted by the TLM is compared to the error growth in Lorenz 63 system for an initial perturbation with standard deviation of 0.1, averaged over 1000 TLM integrations. The is not the error predicted by the TLM, but rather the error of the TLM in predicting the error growth.

2.4 Ensemble Kalman Filters

The computational cost of the EKF is mitigated through the approximation of the error covariance matrix from the model itself, without the use of a TLM.

One such approach is the use of a forecast ensemble, where a collection of models (ensemble members) are used to statistically sample model error propagation. With ensemble members spanning the model analysis error space, the forecasts of these ensemble members are then used to estimate the model forecast error covariance. In the limit of infinite ensemble size, ensemble methods are equivalent to the EKF [Evensen 2003]. There are two prevailing methodologies for maintaining independent ensemble members: (1) adding errors to the observation used by each forecast and assimilating each ensemble individually or (2) distributing ensemble initial conditions from the analysis prediction. In the first method, the random error added to the observation can be truly random [Harris et al. 2011] or be drawn from a distribution related to the analysis covariance. The second method distributes ensemble members around the analysis forecast with a distribution drawn to sample the analysis covariance deterministically. It has been show that the perturbed observation approach introduces additional sampling error that reduces the analysis covariance accuracy and increases the probability of of underestimating analysis error covariance [Hamill et al. 2001]. For the examples given, we demonstrate both methods.

With a finite ensemble size this method is only an approximation and therefore in practice it often fails to capture the full spread of error. To better capture the model variance, additive and multiplicative inflation factors are used to obtain a good estimate of the error covariance matrix (Section 2.6). The spread of ensemble members in the variable of the Lorenz model, as distance from the analysis, can be seen in Figure 2.5.

Figure 2.5: The difference of ensemble forecasts from the analysis is reported for 760 assimilation windows in one model run of length 200, with 10 ensemble members and an assimilation window of length 0.261. This has the same shape of as the difference between ensemble forecasts and the mean of the forecasts (not shown). This spread of ensemble forecasts is what allows us to estimate the error covariance of the forecast model, and appears to be normally distributed.

The only difference between this approach and the EKF, in general, is that the forecast error covariance is computed from the ensemble members, without the need for a tangent linear model:

In computing the error covariance from the ensemble, we wish to add up the error covariance of each forecast with respect to the mean forecast. But this would underestimate the error covariance, since the forecast we’re comparing against was used in the ensemble average (to obtain the mean forecast). Therefore, to compute the error covariance matrix for each forecast, that forecast itself is excluded from the ensemble average forecast.

We can see the classic spaghetti of the ensemble with this filter implemented on Lorenz 63 in Figure 2.6.

Figure 2.6: A sample time-series of the ensembles used in the EnKF. In all tests, as seen here, 10 ensemble members are used. For this run, 384 assimilation cycles were performed with a window length of 0.26 model time units.

We denote the forecast within an ensemble filter as the average of the individual ensemble forecasts, and an explanation for this choice is substantiated by Burgers [Burgers et al. 1998]. The general EnKF which we use is most similar to that of Burgers. Many algorithms based on the EnKF have been proposed and include the Ensemble Transform Kalman Filter (ETKF) [Ott et al. 2004], Ensemble Analysis Filter (EAF) [Anderson 2001], Ensemble Square Root Filter (EnSRF) [Tippett et al. 2003], Local Ensemble Kalman Filter (LEKF) [Ott et al. 2004], and the Local Ensemble Transform Kalman Filter (LETKF) [Hunt et al. 2007]. We explore some of these in the following sections. A comprehensive overview through 2003 is provided by Evensen [Evensen 2003].

2.4.1 Ensemble Transform Kalman Filter (ETKF)

The ETKF introduced by Bishop is one type of square root filter, and we present it here to provide background for the formulation of the LETKF [Bishop et al. 2001]. For a square root filter in general, we begin by writing the covariance matrices as the product of their matrix square roots. Because are symmetric positive-definite (by definition) we can write

(2.29)

for the matrix square roots of respectively. We are not concerned that this decomposition is not unique, and note that must have the same rank as which will prove computationally advantageous. The power of the SRF is now seen as we represent the columns of the matrix as the difference from the ensemble members from the ensemble mean, to avoid forming the full forecast covariance matrix . The ensemble members are updated by applying the model to the states such that an update is performed by

(2.30)

Per [Tippett et al. 2003], the solution for can be solved by perturbed observations

(2.31)

where is the observation perturbation of Gaussian random noise. This gives the analysis with the expected statistics

(2.32)
(2.33)

but as mentioned earlier, this has been shown to decrease the resulting covariance accuracy.

In the SRF approach, the “Potter Method” provides a deterministic update by rewriting

(2.34)
(2.35)
(2.36)

We have defined and . Now for the ETFK step, we use the Sherman-Morrison-Woodbury identity to show

(2.37)

The matrix on the right hand side is practical to compute because it is of dimension of the rank of the ensemble, assuming that the matrix inverse is available. This is the case in our experiment, as the observation are uncorrelated. The analysis update is thus

(2.38)

where is the eigenvalue decomposition of . From [Tippett et al. 2003] we note that the matrix of orthonormal vectors is not unique.

Then the analysis perturbation is calculated from

(2.39)

where and is an arbitrary orthogonal matrix.

In this filter, the analysis perturbations are assumed to be equal to the backgroud perturbations post-multiplied by a transformation matrix so that that the analysis error covariance satisfies

The analysis covariance is also written

where . The analysis perturbations are where .

To summarize, the steps for the ETKF are to (1) form , assuming is easy, and (2) compute its eigenvalue decomposition, and apply it to .

2.4.2 Local Ensemble Kalman Filter (LEKF)

The LEKF implements a strategy that becomes important for large simulations: localization. Namely, the analysis is computed for each grid-point using only local observations, without the need to build matrices that represent the entire analysis space. This localization removes long-distance correlations from and allows greater flexibility in the global analysis by allowing different linear combinations of ensemble members at different spatial locations [Kalnay et al. 2007].

Difficulties are presented however, in the form of computational grid dependence for the localization procedure. The toroidal shape of our experiment, when discretized by OpenFOAM’s mesher and grid numbering optimized for computational bandwidth for solving, does not require that adjacent grid points have adjacent indices. In fact, they are decidedly non-adjacent for certain meshes, with every other index corresponding to opposing sides of the loops. We overcome this difficulty by placing a more stringent requirement on the mesh of localization of indexing, and extracting the adjacency matrix for use in filtering.

The general formulation of the LEKF by Ott [Ott et al. 2004] goes as follows, quoting directly:

  1. Globally advance each ensemble member to the next analysis timestep. Steps 2-5 are performed for each grid point

  2. Create local vectors from each ensemble member

  3. Project that point’s local vectors from each ensemble member into a low dimensional subspace as represented by perturbations from the mean

  4. Perform the data assimilation step to obtain a local analysis mean and covariance

  5. Generate local analysis ensemble of states

  6. Form a new global analysis ensemble from all of the local analyses

  7. Wash, rinse, and repeat.

Figure 2.7 depicts this cycle in greater detail, with similar notations to that used thus far [Ott et al. 2004].

Figure 2.7: The algorithm for the LEKF as described by Ott (2004).

In the reconstructed global analysis from local analyses, since each of the assimilations were performed locally, we cannot be sure that there is any smoothness, or physical balance, between adjacent points. To ensure a unique solution of local analysis perturbations that respects this balance, the prior background forecasts are used to constrain the construction of local analysis perturbations to minimize the difference from the background.

2.4.3 Local Ensemble Transform Kalman Filter (LETKF)

Proposed by Hunt in 2007 with the stated objective of computational efficiency, the LETKF is named from its most similar algorithms from which it draws [Hunt et al. 2007]. With the formulation of the LEKF and the ETKF given, the LETKF can be described as a synthesis of the advantages of both of these approaches. This is the method that was sufficiently efficient for implementation on the full OpenFOAM CFD model of 240,000 model variables, and so we present it in more detail and follow the notation of Hunt et al (2007). As in the LEKF, we explicitly perform the analysis for each grid point of the model. The choice of observations to use for each grid point can be selected a priori, and tuned adaptively. The simplest choice is to define a radius of influence for each point, and use observations within that. In addition to this simple scheme, Hunt proposes weighing observations by their proximity to smoothly transition across them. The goal is to avoid sharp boundaries between neighboring points.

Regarding the LETKF analysis problem as the construction of an analysis ensemble from the background ensemble, where we specify that the mean of the analysis ensemble minimizes a cost function, we state the equations in terms of a cost function. The LETKF is thus

(2.40)

where

Since we have defined for the matrix , the rank of is at most , and the inverse of is not defined. To ameliorate this, we consider the analysis computation to take place in the subspace spanned by the columns of (the ensemble states), and regard as a linear transformation from a -dimensional space into . Letting be a vector in , then belongs to and . We can therefore write the cost function as

and it has been shown that this is an equivalent formulation by [Hunt et al. 2007].

Finally, we linearize by applying it to each and interpolating. This is accomplished by defining

(2.41)

such that

(2.42)

where is the matrix whose columns are for the average of the over . Now we rewrite the cost function for the linearize observation operator as

This cost function minimum is the form of the Kalman Filter as we have written it before:

In model space these are

We move directly to a detailed description of the computational implementation of this filter. Starting with a collection of background forecast vectors , we perform steps 1 and 2 in a global variable space, then steps 3-8 for each grid point:

  1. apply to to form , average the for , and form .

  2. similarly form . (now for each grid point)

  3. form the local vectors

  4. compute (perhaps by solving

  5. compute where is a tunable covariance inflation factor

  6. compute

  7. compute and add it to the column of

  8. multiply by each and add to get to complete each grid point

  9. combine all of the local analysis into the global analysis

The greatest implementation difficulty in the OpenFOAM model comes back to the spatial discretization and defining the local vectors for each grid point.

Four Dimensional Local Ensemble Transform Kalman Filter (4D-LETKF)

We expect that extending the LETKF to incorporate observations from within the assimilation time window will become useful in the context of our target experiment high-frequency temperature sensors. This is implemented without great difficulty on top of the LETKF, by projecting observations as they are made into the space with the observation time-specific matrix and concatenating each successive observation onto . Then with the background forecast at the time , we compute and , concatenating onto and , respectively.

2.5 4D-Var

The formulation of 4D-Var aims to incorporate observations at the time they are observed. This inclusion of observations has resulted in significant improvements in forecast skill, cite. The next generation of supercomputers that will be used in numerical weather prediction will allow for increased model resolution. The main issues with the 4D-Var approach include attempting to parallelize what is otherwise a sequential algorithm, and the computational difficulty of the strong-constraint formulation with many TLM integrations, with work being done by Fisher and Andersson (2001). The formulation of 4D-Var is not so different from 3D-Var, with the inclusion of a TLM and adjoint model to assimilation observations made within the assimilation window. At the ECMWF, 4D-Var is run on a long-window cycle (24 and 48 hours) so that many observations are made within the time window. Generally, there are two main 4D-Var formulations in use: strong-constraint and weak-constaint. The strong-constraint formulation uses the forecast model as a strong constraint, and is therefore easier to solve. From Kalnay (2007) we have the standard weak-constaint formulation with superscript denoting the timestep within the assimilation window (say there are observation time steps within the assimilation window):

The weak-constraint formulation has only recently been implemented operationally. This is [Kalnay et al. 2007]:

Future directions of operational data assimilation combine what is best about 4D-Var and ensemble-based algorithms, and these methods are reffered to as ensemble-variational hybrids. We have already discussed a few such related approaches: the use of the Kalman gain matrix used within the 3D-Var cost function, the “NCEP” method for 3D-Var, and inflating the ETKF covariance with the 3D-Var static (climatological) covariance .

2.5.1 Ensemble-variational hybrids

Ensemble-variational hybrid approaches benefit from flow dependent covariance estimates obtained from an ensemble method, and the computational efficiency of iteratively solving a cost function to obtain the analysis, are combined. An ensemble of forecasts is used to update the static error covariance in the formulation of 4D-Var (this could be done in 3D-Var as well) with some weighting from the climatological covariance and the ensemble covariance. This amounts to a formulation of

(2.43)

for some between 0 and 1. Combining the static error covariance and the flow dependent error covariance is an active area of research [Clayton et al. 2012].

2.6 Performance with Lorenz 63

With the EKF, EnKF, ETKF, and EnSRF algorithms coded as above, we present some basic results on their performance. First, we see that using a data assimilation algorithm is highly advantageous in general (Figure 2.8). Of course we could think to use the observations directly when DA is not used, but since we only observing the variable (and in real situations measurements are not so direct), this is not prudent.

Figure 2.8: For near-perfect initial knowledge of the atmospheric state, the running average RMS error of a prediction using DA is compared against a prediction that does not. Initial error for DA is normal with mean 0 and variance 0.01, and the RMS errors reported are averages of 3 runs. Observational noise is normally distributed with mean 0 and variance 0.05 (approximately 5% of climatological variation), and an assimilation window length of 0.25 is used. As would be expected, in the long run DA greatly improves forecast skill, as forecasts without DA saturate to climatological error. The initial period where a forecast exceeds the skill of DA is potentially due to the spin-up time required by the filter to dial in the analysis error covariance.

Next, we test the performance of each filter against increasing assimilation window length. As we would expect, longer windows make forecasting more challenging for both algorithms. The ensemble filter begins to out-perform the extended Kalman filter for longer window lengths because the ensemble more accurately captures the nonlinearity of the model.

Figure 2.9: The RMS error (not scaled by climatology) is reported for our EKF and EnKF filters, measured as the difference between forecast and truth at the end of an assimiliation window for the latter 2500 assimiliation windows in a 3000 assimilation window model run. Error is measured in the only observed variable, . Increasing the assimilation window led to an decrease in predictive skill, as expected. Additive and multiplicative covariance inflation is the same as Harris et. al (2011).

Each of the filters is sensitive to the size of the covariance matrix, and in some cases to maintain the numerical stability of the assimilation it is necessary to use additive and/or multiplicative covariance inflation. In all filters multiplicative error is performed with inflation factor by

(2.44)

Additive inflation is performed for the EKF as in Yang et al (2006) and Harris et al (2011) where uniformly distributed random numbers in are added to the diagonal. This is accomplished in MATLAB by drawing a vector of length of uniformly distributed numbers in , multiplying it by , and adding it to the diagonal:

(2.45)

For the EnKF we perform additive covariance inflation to the analysis state itself for each ensemble:

(2.46)

The result of searching over these parameters for the optimal values to minimize the analysis RMS error differs for each window length, so here here we present the result for a window of length 390 seconds for the ETKF. In Figure 2.10 we see that there is a clear region of parameter space for which the filter performs with lower RMS, although this region appears to extend into values of .

Figure 2.10: The RMS error averaged over 100 model runs of length 1000 windows is reported for the ETKF for varying additive and multiplicative inflation factors and . Each of the 100 model runs starts with a random IC, and the analysis forecast starts randomly. The window length here is 390 seconds. The filter performance RMS is computed as the RMS value of the difference between forecast and truth at the assimilation window for the latter 500 windows, allowing a spin-up of 500 windows.

Chapter 3 Thermal Convection Loop Experiment

The thermosyphon, a type of natural convection loop or non-mechanical heat pump, can be likened to a toy model of climate [Harris et al. 2011]. In this chapter we present both physical and computationally simulated thermosyphons, the equations governing their behavior, and results of the computational experiment.

3.1 Physical Thermal Convection Loops

Under certain conditions, thermal convection loops operate as non-mechanical heat pumps, making them useful in many applications. In Figures 3.3 and 3.2 we see four such applications. Solar hot water heaters warm water using the sun’s energy, resulting in a substantial energy savings in solar-rich areas [Carlton 2009]. Geothermal systems heat and cool buildings with the Earth’s warmth deep underground, and due to low temperature differences are often augmented with a physical pump. CPU coolers allow modern computers to operate at high clock rates, while reducing the noise and energy consumption of fans [Bernhard 2005]. Ground thermosyphons transfer heat away from buildings built on fragile permafrost, which would otherwise melt in response to a warming climate, and destroy the building [Xu and Goering 2008]. The author notes that these systems rely on natural convection, and when augmented with pumps the convection is mixed or forced, and would necessitate different models.

Figure 3.1: Here we see many different thermosyphon applications. Clockwise starting at the top, we have a geothermal heat exchanger, solar hot water heater, and computer cooler. Images credit to BTF Solar and Kuemel Bernhard [Bernhard 2005, Carlton 2009].
Figure 3.2: Thermosyphons flank a Federal Aviation Administration building in Fairbanks, Alaska. The devices help keep the permafrost frozen beneath buildings and infrastructure by transferring heat out of the ground. Photo credit Jim Carlton [Carlton 2009].

3.1.1 Ehrhard-Müller Equations

Figure 3.3: Schematic of the experimental, and computational, setup from Harris et al (2012). The loop radius is given by and inner radius by . The top temperature is labeled and bottom temperature , gravity is defined downward, the angle is prescribed from the 6 o’clock position, and temperature difference is labeled.

The reduced order system describing a thermal convection loop was originally derived by Gorman [Gorman et al. 1986] and Ehrhard and Müller [Ehrhard and Müller 1990]. Here we present this three dimensional system in non-dimensionalized form. In Appendix B we present a more complete derivation of these equations, following the derivation of Harris [Harris et al. 2011]. For the mean fluid velocity, temperature different , and deviation from conductive temperature profile, respectively, these equations are:

(3.1)
(3.2)
(3.3)

The parameters and , along with scaling factors for time and each model variable can be fit to data using standard parameter estimation techniques.

Tests of the data assimilation algorithms in Chapter 2 were performed with the Lorenz 63 system, which is analogous to the above equations with Lorenz’s , and . From these tests, we have found the optimal data assimilation parameters (inflation factors) for predicting time-series with this system. We focus our efforts on making prediction using computational fluid dynamics models. For a more complete attempt to predict thermosyphon flow reversals using this reduced order system, see the work of Harris et al (2012).

3.1.2 Experimental Setup

Figure 3.4: A time series of the physical thermosyphon, from the Undergraduate Honor’s Thesis of Darcy Glenn [Glenn 2013]. The temperature difference (plotted) is taken as the difference between temperature sensors in the 3 and 9 o’clock positions. The sign of the temperature difference indicates the flow direction, where positive values are clockwise flow.
Figure 3.5: The Thermal Convection Loop experiment, inlaid with a time series of the temperature difference whose sign indicates the flow direction. Fluorescent balls are lit by a black-light and move with the flow. As the timeseries indicates, the flow changes direction aperiodically, giving rise to the chaotic behavior that we model. A video of the loop, from which this is a snapshot, can be viewed at http://www.youtube.com/watch?feature=player_embedded&v=Vbni-7veJ-c.

Originally built (and subsequently melted) by Dr. Chris Danforth at Bates College, the University of Vermont maintains experimental thermosyphons. Operated by Dave Hammond, UVM’s Scientific Electronics Technician, the experimental thermosyphons access the chaotic regime of state space found in the principled governing equations. We quote the detailed setup from Darcy Glenn’s undergraduate thesis [Glenn 2013]:

The [thermosyphon] was a bent semi-flexible plastic tube with a 10-foot heating rope wrapped around the bottom half of the upright circle. The tubing used was light-transmitting clear THV from McMaster-Carr, with an inner diameter of 7/8 inch, a wall thickness of 1/16 inch, and a maximum operating temperature of 200F. The outer diameter of the circular thermosyphon was 32.25 inches. This produced a ratio of about 1:36 inner tubing radius to outside thermosyphon radius (Danforth 2001). There were 1 inch ’windows’ when the heating cable was coiled in a helix pattern around the outside of the tube, so the heating is not exactly uniform. The bottom half was then insulated using aluminum foil, which allowed fluid in the bottom half to reach 176F. A forcing of 57 V, or 105 Watts, was required for the heating cable so that chaotic motion was observed. Temperature was measured at the 3 o’clock and 9 o’clock positions using unsheathed copper thermocouples from Omega.

We first test our ability to predict this experimental thermosyphon using synthetic data, and describe the data in more detail in Chapter 4. Synthetic data tests are the first step, since the data being predicted is generated by the predictive model. We consider the potential of up to 32 synthetic temperature sensors in the loop, and velocity reconstruction from particle tracking, to gain insight into which observations will make prediction possible.

3.2 Computational Experiment

In this section, we first present the governing equations for the flow in our thermal convection loop experiment. A spatial and temporal discretization of the governing equations is then necessary so that they may be solved numerically. After discretization, we must specify the boundary conditions. With the mesh and boundary conditions in place, we can then simulate the flow with a computational fluid dynamics solver.

We now discuss the equations, mesh, boundary conditions, and solver in more detail. With these considerations, we present our simulations of the thermosyphon.

3.2.1 Governing Equations

We consider the incompressible Navier-Stokes equations with the Boussinesq approximation to model the flow of water inside a thermal convection loop. Here we present the main equations that are solved numerically, noting the assumptions that were necessary in their derivation. In Appendix C a more complete derivation of the equations governing the fluid flow, and the numerical for our problem, is presented. In standard notation, for the velocity in the direction, respectively, the continuity equation for an incompressible fluid is

(3.4)

The momentum equations, presented compactly in tensor notation with bars representing averaged quantities, are given by

(3.5)

for the reference density, the density from the Boussinesq approximation, the pressure, the viscocity, and gravity in the -direction. Note that for since gravity is assumed to be the direction. The energy equation is given by

(3.6)

for the total internal energy and the flux (where is the averaging notation).

Figure 3.6: A snapshot of the mesh used for CFD simulations. Shown is an initial stage of heating for a fixed value boundary condition, 2D, laminar simulation with a mesh of 40000 cells including wall refinement with walls heated at 340K on the bottom half and cooled to 290K on the top half.

3.2.2 Mesh

Creating a suitable mesh is necessary to make an accurate simulation. Both 2-dimensional and 3-dimensional meshes were created using OpenFOAM’s native meshing utility “blockMesh.” After creating a mesh, we consider refining the mesh near the walls to capture boundary layer phenomena and renumbering the mesh for solving speed. To refine the mesh near walls, we used the “refineWallMesh” utility, Lastly, the mesh is renumbered using the “renumberMesh” utility, which implements the Cuthill-McKee algorithm to minimize the adjacency matrix bandwidth, defined as the maximum distance from diagonal of nonzero entry. The 2D mesh contains 40,000 points, and is imposed with fixed value boundary conditions on the top and bottom of the loop.

Figure 3.7: The 3D mesh viewed as a wireframe from within. Here there are 900 cells in each slice (not shown), for a total mesh size of 81,000 cells. Simulations using this computational mesh are prohibitively expensive for use in a real time ensemble forecasting system, but are possible offline.
Figure 3.8: The 2D mesh Adjacency matrix for a local radius of 1.0cm. In general, we see that cells have neighbors with nearby cell ID. With 5,260,080 nonzero entries, it is difficult to see structure looking at the entire matrix. This figure was bitmapped for inclusion on the arXiv, for a full version see http://andyreagan.com.
Figure 3.9: The 2D mesh adjacency matrix, zoomed in. The Cuthill-McKee renumbering algorithm was used, and we see 23 distinct regions of local numbering, reflective of the geometry and Cuthill-McKee algorithm. The mesh shown here has 30 cells in each perpendicular slice of the loop, and they are numbered iteratively along the edge of triangular front emanating from cell 0 (chose to be the left-most cell). This diagonalization in both space and ID number effectively reduces the bandwidth of the mesh from 947 to 18. This figure was bitmapped for inclusion on the arXiv, for a full version see http://andyreagan.com.

3.2.3 Boundary Conditions

Available boundary conditions (BCs) that were found to be stable in OpenFOAM’s solver were constant gradient, fixed value conditions, and turbulent heat flux. Simulations with a fixed flux BC is implemented through the externalWallHeatFluxTemperature library were unstable and resulted in physically unrealistic results. Constant gradient simulations were stable, but the behavior was empirically different from our physical system. Results from attempts at implementing these various boundary conditions are presented in Table 3.1. To most accurately model our experiment, we choose a fixed value BC. This is due to the thermal diffusivity and thickness of the walls of the experimental setup. For the flow of heat from the hot water bath into the loop’s outer material, and the area of a small section of boundary we can write the heat flux into the fluid inside the loop as a function of the thermal conductivity , temperature difference and wall thickness :

(3.7)

For our experimental setup, the thermal conductivity of a PVC wall is approximately . With a wall thickness of 1cm, and the heat flux is . The numerical implementation of this boundary condition is considered further in Appendix C. In Table 3.1 we list the boundaries conditions with which we experimented, and the quality of the resulting simulation.

Boundary Condition Type Values Considered Result
fixedValue value realistic
fixedGradient gradient plausible
wallHeatTransfer enthalpy - cannot compile
externalWallHeatFluxTemperature flux - cannot compile
turbulentHeatFluxTemperature flux unrealistic
Table 3.1: Boundary conditions considered for the OpenFOAM CFD model are labeled with their type, values considered, and empirical result. We find the most physically realistic simulations using the simplest “fixedValue” condition. The most complex conditions, “wallHeatTransfer,” “externalWallHeatFluxTemperature,” and “turbulentHeatFluxTemperature” either did not compile or produced divergent results.

3.2.4 Solver

In general, there are three approaches to the numerical solution of PDEs: finite differences, finite elements, and finite volumes. We perform our computational fluid dynamics simulation of the thermosyphon using the open-source software OpenFOAM. OpenFOAM has the capacity for each scheme, and for our problem with an unstructured mesh, the finite volume method is the simplest. The solver in OpenFOAM that we use, with some modification, is “buoyantBoussinesqPimpleFoam.” Solving is accomplished by the Pressure-Implicit Split Operator (PISO) algorithm [Issa 1986]. Modification of the code was necessary for laminar operation. In Table 3.2, we note the choices of schemes for time-stepping, numerical methods and interpolation.

The Boussinesq approximation makes the assumption that density changes due to temperature differences are sufficiently small so that they can be neglected without effecting the flow, except when multiplied by gravity. The non-dimensionalized density difference depends on the value of heat flux into the loop, but remains small even for large values of flux. Below, we approximate the validity of the Boussinesq approximation, which is generally valid for values of :

(3.8)
Problem Scheme
Main solver buoyantBoussinesqPimpleFoam
Solving algorithm PISO
Grid Semi-staggered
Turbulence model None (laminar)
Time stepping Euler
Gradient Gauss linear
Divergence Gauss upwind
Laplacian Gauss linear
Interpolation Linear
Matrix preconditioner Diagonal LU
Matrix solver Preconditioned Bi-linear Conjugate Gradient
Table 3.2: Numerical schemes used for solving the finite volume problem.

3.2.5 Simulation results

With the mesh, BCs, and solver chosen, we now simulate the flow. From the data of and that are saved at each timestep, we extract the mass flow rate and average temperature at the and o’clock positions on the loop. Since is saved as a face-value flux, we compute the mass flow rate over the cells of top (12 o’clock) slice as