 Research
 Open Access
Modelling, asymptotic analysis and simulation of the gas dynamics in a chimney
 Elisabetta Felaco^{1} and
 Ingenuin Gasser^{1}Email author
https://doi.org/10.1186/2190598333
© Felaco and Gasser; licensee Springer 2013
 Received: 3 January 2012
 Accepted: 1 July 2013
 Published: 8 July 2013
Abstract
This paper presents a one dimensional model for the gas dynamics in a chimney. This is a prototype example of a small Mach number flow with strong heat sources. Due to the small Mach number of the gas flow an asymptotic model is derived from a fully compressible model, which then is compared to the original model and to the often used Boussinesq approximation. The Boussinesq approximation is shown to be inappropriate for this application, whereas the small Mach number asymptotic model we propose is shown to be a very good approximation. In particular it allows very fast numerical simulations. Finally, all this is underlined by numerical simulations where we validate the various models.
MSC:35C20, 35Q35, 76M45, 76N15, 80A20.
Keywords
 chimney
 gas dynamics
 Low Mach number
 Boussinesq approximation
1 Introduction
Chimneys are typical representatives of the beginning of the industrial era in the 18th century. However there is a much longer story behind. Starting from the 13th century chimneys were build and used to channel away smoke and hot air. Nowadays chimneys are common presences in our everyday life, from industrial applications to the heating systems in our houses. Just to give some examples, we can think to modern heating systems, whit different kinds of fuel, and also to Controlled Ventilation Systems, where the basic principle of chimney is used, often with the help of a fan, to keep an healthy level of oxygen in modern buildings [1].
Here by chimney we mean a vertical structure for venting into the outside atmosphere hot flue gases produced e.g. in a combustion process like in a boiler, in a stove, in a furnace or in a fireplace. The underlying main physical principles are well understood. Therefore it is considered only a technical issue to give precise and quantitative predictions of the gas dynamics in a chimney. On one hand there is huge technological know how (for example see [2] and [3]) with empirical formulas for very specific situations based on restrictive (often unrealistic) assumptions. On the other hand one can find sophisticated CFD gasdynamics simulations based on time expensive numerical simulations. There seems to be a peculiar lack of models in between these two extreme areas, i.e. models which are physically reasonably realistic and numerically cheap at the same time. This paper goes exactly in this direction.
When describing the gas dynamics in a chimney a few crucial facts can be identified.

The flow is driven by density gradients (buoyancy force).

The flow velocities are slow compared to the speed of sound.

The temperature differences are big and decisive for the flow behaviour.
Small flow velocities indicate an incompressible model. In combination with the buoyancy as driving force a model with variable density is necessary. In such a context a widely used approach is the Boussinesq approximation going back originally to Boussinesq [4] with later justifications by Bois, Zeytounian etc. (see e.g. [5–7] and citations therein). However we will show that here a Boussinesq type approach is not appropriate. As an alternative we use a variable density low Mach number model (see [8–12] for the non isentropic or the non isothermal cases) adapted to this approximation which results to be realistic and numerically cheap at the same time.
The aim of the paper is to study the flow dynamics both qualitatively and quantitatively. A common measure for the quality of the full process in a chimney is the draft in the chimney. And the draft in the chimney depends e.g. on the heat source, on the chimney geometry, on the chimney friction and heat loss parameters, on the outside meteorological situation etc.
In Section 2 we describe the underlying equations. In Section 3 we will scale the equation and identify various asymptotic regions. In Section 4 we discuss the non validity of a Boussinesq type model and propose a variable density low Mach number model. Finally in Section 5 we will provide several numerical examples, first using simulations on a full system of equations as a reference to underline the validity of our approach, and then analysing in more details the dependence on the parameters.
2 The model
The fresh cold air enters at the base of the structure and, after flowing through a small section of the chimney, it reaches the fireplace. There a combustion process takes place and the air gains some heat and mass (in the combustion process the air mixture typically looses oxygen and gains carbon dioxide and water vapor, the total variation resulting in an net increase of the air mass). As a result the density decreases and the velocity increases. The hot air smoke mixture enters the main part of the chimney, where the so called chimney effect acts as the main driving force. Clearly, in that part there are also other effects like friction and heat losses. Finally the hot air smoke mixture exits at the top of the structure.
We assume that the main dynamics acts in vertical direction, as we do not expect significant flow phenomena in other directions. Then almost all gas particles experience the same when passing through the structure. Therefore we describe the gas dynamics by a one dimensional model, where the single dimension x starts at the base of the structure and follows the air flow towards the top of the chimney. All quantities under consideration have to be interpreted as mean values over the cross sectional area. However, this approach still allows to consider variable cross sections e.g. a larger cross section in the fire place area.
In (1) the term on the right hand side $\tilde{m}$ is due to the additionally produced gas in the combustion process as a consequence of the oxygen consumption. We will propose a model for this mass variation in the next section.
is the so called hydraulic diameter. Realistic values for λ can be found in literature, see, for example [13].
In case of an additional fan (for example in low temperature chimneys) a pressure gain term $\tilde{\mathrm{\Delta}}{p}_{fan}/L$ is introduced, where L is the reference value for the length of the chimney.
where $St=\lambda /8$ is the Stanton number [14]. Using average density and velocity values we can compute α. Note that in Section 5 we will use slightly smaller α values to take into account the presence of insulating materials typically used in chimney walls [2, 3, 15, 16].
Finally $\sigma =5.670400\times {10}^{8}{\text{J s}}^{1}{\text{m}}^{2}{\text{K}}^{4}$ is the thermal radiation coefficient (Stefan’s constant).
2.1 Modelling the mass loss and the heat source
where ${\tilde{c}}_{m}$ and ${\tilde{c}}_{q}$ are a mass variation and a heat production coefficient. To determine reasonable values to these coefficients we recall that burning wood produces ∼10^{6} J/kg of thermal energy ([17, 18] and [19]), while chimneys used for heating in common handholds have usually a power of 10^{2} kW [15, 16]. Considering this and taking into account the reference values for density and velocity, we will use a heat production coefficient ${\tilde{c}}_{q}\sim {10}^{5}\text{\u2013}{10}^{6}{\text{kg m/s}}^{2}$.
As for the mass variation in the air, there are different possible approaches [20]. We can consider the burning reaction and compare the wood mass loss with the mass gain in the air, and then use the results from [18] and [19]. Otherwise we can use the experimental results on the oxygen variation in air after combustion. We will use ${\tilde{c}}_{m}\sim {10}^{2}$ 1/m.
3 Scaling
Scaling table with typical reference values
Quantity  Reference value  Typical reference value 

x  ${x}_{r}=L$  10 m 
t  ${t}_{r}$  20 s 
A  ${A}_{r}$  0.07 m^{2} 
h  L  10 m 
u  ${u}_{r}=L/{t}_{r}$  0.5 m/s 
p  ${p}_{r}$  101,328 kg/(m s^{2}) 
T  ${T}_{r}={T}_{w}$  263 K (=−10^{∘}C) 
ρ  ${\rho}_{r}={p}_{r}/(R{T}_{r})$  1.3 kg/m^{3} 
q  ${q}_{r}={\tilde{c}}_{q}{\rho}_{r}{u}_{r}$  5 × 10^{5} W/m^{3} 
m  ${m}_{r}={\tilde{c}}_{m}{\rho}_{r}{u}_{r}$  5 × 10^{−2} kg/(s m^{3}) 
(Here ${\rho}_{r}:={p}_{r}/R{T}_{r}$, see Table 1.)
Constants
Constant  Value 

g  9.81 m/s^{2} 
R  287 m^{2}/(s^{2} K) 
${c}_{v}$  718 m^{2}/(s^{2} K) 
γ  1.4 
σ  5.6704 × 10^{−8} J s^{−1} m^{−2} K^{−4} 
We note that in our setting $M\sim {10}^{3}$ and therefore $\frac{1}{{M}^{2}}\sim {10}^{6}$. In addition we have $Fr\sim {10}^{1}$ and therefore $\frac{1}{F{r}^{2}}\sim {10}^{2}$. These facts suggest to perform an asymptotic analysis with the intention to further simplify the model.
3.1 Initial and boundary conditions
where ${p}_{l}$ and ${p}_{r}$ are, respectively, pressure at the bottom and pressure at the top of the structure.
Remember that in a vertical setting the height is $h(x)=x$, $x=0$ at the bottom, x axis oriented toward the top of the chimney. In our scaling the values at the bottom are given by ${\rho}_{h0}=1$ and ${p}_{h0}=1$.
Thus the problem to solve consists of the equations (4)(7), the initial conditions (8), the boundary condition (9) and (10) specified in (15) and (16).
4 Asymptotics
should not be ruled out. The case (17) leads to the so called Boussinesq approximation, the case (18) is known as the small Mach number limit. Both approximations are widely used, see [4–7] and citations therein for the Boussinesq approximation. For the small Mach number approximation in general (non isentropic and non isothermal) see [8–12, 22], for numerical issues see [23–26] and references therein. For a variety of one dimensional applications similar to the one in this paper see [27–30]. In the literature (for example in [31]) the Boussinesq number is defined as $B={M}^{2}/F{r}^{2}$. Both cases (17) and (18) refer to the limit $B\to 0$, whereas the quasistatic case would correspond to a limit with $B\to {B}_{0}\ne 0$.
In the following for sake of simplicity we neglect the terms involving the fan and the radiation energy. Also, we deal with a vertical chimney such that $h(x)=x$ holds. We start with the classical Boussinesq approximation.
4.1 Boussinesq approximation
to obtain in (4)(6) a hierarchy of equations.
This means that a mass loss or a heat source of order one is not compatible with the Boussinesq assumption of a constant leading order density. This is reasonable since order one mass loss or heat source terms are supposed to induce significant order one changes in the density (and therefore in temperature). We conclude that the Boussinesq approximation is NOT applicable in our case of significant mass losses or heat source. Therefore in Section 4.2 we pass to the small Mach number asypmtotics.
the Boussinesq approximation would be applicable and we obtain the well known ‘incompressibility’ condition ${u}_{x}^{(0)}=0$ and a ${u}^{(0)}={u}^{(0)}(t)$. Then (20) and (25) become the two equations for the perturbations ${u}^{(1)}$ and ${\rho}^{(1)}$. Finally ${\rho}^{(1)}$ enters in the buoyancy term on the right hand side of (23).
which are exactly the first two terms in the expansion of the adiabatic formula (12) for the density. In Section 5.2 we come back to these asymptotics when doing numerical comparisons.
Remark 2 We said that this derivation of the Boussinesq approximation is in the line of [7] which is different from the more classical asymptotic derivations going back to [5, 6]. In fact in [5, 6] a multiple scale analysis is used to obtain the final equations. However, the non applicability of the Boussinesq approximation in our application is independent of the chosen approach. For details on the differences between the approaches see [7].
4.2 Small Mach number approximation
Here we keep the Froude number Fr fixed and consider only the Mach number to be small. This limit is well known (see citations at the beginning of this section). Note again that from the state equation we get $T=p/\rho $ so that we consider only the equations (4)(6) for the unknowns ρ, p and u.
where we used ${T}^{(0)}={p}^{(0)}/{\rho}^{(0)}$.
These equations have to be completed with initial data for ${\rho}^{(0)}$, ${u}^{(0)}$ and boundary conditions (30) for ${p}^{(2)}$ and (31) for ${\rho}^{(0)}$.
Note that ${\rho}^{(0)}$ is not constant and describes eventually big density changes which imply big temperature changes. The same holds for ${u}^{(0)}$. Contrary to the Boussinesq approximation we encounter no contradiction with order one mass loss or heat source terms. Therefore we proceed with this set of equations in the following sections.
As we can see in (32)(34), the model contains 4 parameters which have to be chosen appropriately, i.e. ${c}_{m}$, ${c}_{q}$, ξ and a. The former two parameters depend on the chemistry of the fire, the latter two (friction and heat loss) only on the construction of the chimney. The quality of quantitative results obtained by this model depends on the precision of knowledge of the 4 mentioned parameters. By the way, this problem is in common with all approaches, in particular also with all the sophisticated CFD ones. The model, being 1 dimensional and not fully compressible, allows  as we will see also in the examples  fast simulations. Fast direct simulations are the basis of any optimisation strategy. In the planning stage of a chimney the diameter of the chimney, the height of the chimney, the size of the allowed heat loss etc. are typical parameters to be optimised.
5 Numerical simulations
5.1 A reformulation of the small Mach number equations
We are now interested in solving numerically equations (32)(34) with initial data (8) for ${\rho}^{(0)}$ and ${u}^{(0)}$, boundary conditions (30) for ${p}^{(2)}$ and inflow conditions (31) for ${\rho}^{(0)}$.
where we dropped the index ${(0)}^{}$ for ${\rho}^{(0)}$ and ${u}^{(0)}$. The boundary conditions for the altitude corrected pressure are given by ${p}^{ac}(0,t)={p}^{ac}(1,t)=0$. From now on we drop the superscript ac.
Also, here we included again the additional fan and the radiation term, that were previously neglected for sake of simplicity.
We reformulate (35)(37) in order to simplify and in particular to obtain a system of evolution equations. First we integrate (37) in space on $(0,x)$, and define a new function $v(t):=A(0)u(0,t)$; then we rewrite (35) using (37); finally we integrate (36) in space on $(0,1)$.
where $\mathrm{\Delta}{p}^{(2)}=({p}^{(2)}(1,t){p}^{(2)}(0,t))=0$.
Thus we have to solve a PDE for the density $\rho (x,t)$, an ODE for $v(t)$, both evolution equations, and an integral equation for $u(x,t)$.
Finally we have to discuss how the initial, boundary and inflow conditions translate in terms of these new equations.
The initial data (8) can be transformed in initial data for equations (39)(40), while the boundary conditions for the pressure are included in equation (40). The inflow conditions (31) for the density stay unaltered.
To solve equations (38), (39) and (40) we use

an explicit upwind for the PDE for ρ in (39),

an explicit time step for the ODE for v in (40),

an explicit time step for the integral equation for u in (38).
where ${F}_{u}$, ${F}_{\rho}$, ${F}_{v}$ are the right hand sides of (38), (39), (40), respectively.
The integrals involved are solved by summation. To use $\frac{({u}_{i}^{n}{u}_{i}^{n1})}{\mathrm{\Delta}t}$ at the starting time (level $n=0$), we prescribe (the same) initial values for u also at a level $n=1$.
To assure stability of the scheme we only need to check CFL condition for the upwind scheme. This method is the simplest reasonable choice (from a numerical point of view) and promises to be fast. We will see that this simple choice already guarantees numerical robustness. In the future we plan to study more sophisticated numerical approaches to simulate our set of equations.
To be more precise we expect to be (much) faster than the corresponding simulations on the full set of compressible equations (4)(6). This is due to the fact that the CFL condition in the compressible equations (4)(6) is very restrictive due to big sound speed (due to the small Mach number). Contrary to that the CFL condition in (40)(39) is determined by the flow velocity (which is of order one) and allows much bigger time steps. In addition every time step in the asymptotic model consists of an ODE and a single PDE timestep, whereas in the fully compressible model we have a time step in a coupled system of three PDE’s. In a similar context a precise comparison of the numerical effort was presented [29].
Geometrical data
Value  

Chimney length before the fire place  0.5 m 
Fire place height  0.5 m 
Chimney length after the fire place  7 m 
Chimney radius  0.125 m 
Fireplace radius  0.25 m 
We will run our simulations with final time $T=20$ s since within this time range the stationary state is reached in all our examples.
5.2 Example 1: Basic description  comparisons with other models
At first we would like to compare the results obtained from our model, with those obtained from the Boussinesq approximation (19)(25) and from the full system (4)(7), which will be used as our reference.
Here $\mathrm{\Delta}{p}^{(2)}=({p}^{(2)}(1,t){p}^{(2)}(0,t))=0$, where we used the altitude corrected pressure; the boundary conditions are those obtained in Section 4.1. To solve these equations we use an explicit upwind scheme for ${\rho}^{(1)}$ and an explicit time step for ${u}^{(0)}$.
In order to solve the full system (4)(7), we use the standard technique of splitting the problem into two subproblems, solving first the hyperbolic conservation law by an upwind scheme, and then solving the ODE for the source term with an explicit Euler scheme. In this case, we choose to use a first order scheme in order to have a reasonable comparison with the result obtained from the other two models.
Data for basic examples
Symbol  Value  

Friction factor  λ  1 
Heat loss coefficient  α  0 
Constant for heat exchange  ${\tilde{c}}_{q}$  6 × 10^{5} kg m/s^{2} 
Constant for mass loss  ${\tilde{c}}_{m}$  10^{−2} m 
Wall temperature  ${T}_{w}$  −10^{∘}C 
As for the initial data, we consider ${u}_{0}(x)\equiv 0$, ${\rho}_{0}(x)={\rho}_{h}(x)$ and, in the case of the full system, ${p}_{0}(x)={p}_{h}(x)$.
After a simulation time of few seconds, all three models reach stationary values, and we can compare the result for velocity, density and temperature of air through the chimney.
In Figure 2 after a first period where the density is still positive (and positive temperature), also the temperature becomes negative due to (44). This is not a numerical problem, but a problem of the wrong asymptotics. The reason is that for strong heat sources the Boussinesq approximation is a bad approximation since the higher order terms in the asymptotics are not of higher order but of the same order as the leading order terms.
On the other hand, lowering the heat sources, the Boussinesq approximation becomes reasonable, in the sense that the density and the temperature are no more negative.
5.3 Example 1.2: adding heat loss
Now we concentrate on the results obtained with our model.
This choice is motivated by the fact that many chimneys are not isolated over the last meters (at least in older buildings) since there the chimney passes under the roof (which may be a not heated area) or even outside of the roof. In the heated part of the building chimneys are typically well isolated.
As we can see from Figure 6, when the air flow passes the fireplace, temperature increases (as density decreases). The wider cross section in the fireplace reduces the velocity. The stationary state is reached very rapidly.
The maximal velocity and maximal temperature are, respectively, 2 m/s and 240^{∘}C, while at the top of the chimney, the exit velocity is about 1.8 m/s and the exit temperature is about 155^{∘}C. All these are reasonable values. In modern chimneys, thanks to the use of special materials, the friction factor and the heat loss coefficient are kept considerably smaller, such that for small heat sources there is still a good draft.
We finally note that adding the radiation term in the energy equation does not affect the previous results since the Stefan constant is too small. Or in other words, the reached temperature is too low to induce significant losses due to radiation.
5.4 Example 2: effects of the geometry
Here we show how the draft velocity depends  for fixed cross sectional area at the fireplace  on the geometry of the structure.
5.5 Example 3: dependence on the friction factor
5.6 Example 4: external influences
Finally we model the presence of strong winds on the chimney top that may interfere with the hot gas flowing out of the structure.
We assume that the pressure variation at the top of the chimney due to wind refers mainly to horizontal wind directions. In case of a vertical wind component there would be an influence on the direction of the vertical part of the velocity but, thanks to rotational symmetry, no influence on the direction of the horizontal part is expected.
So we simulate the outside wind by increasing the external pressure.
6 Conclusions
This paper proposes a small Mach number model to describe the gas dynamics in a chimney. It is shown that in this small Mach number application with strong heat sources the Boussinesq approach is not adequate. However, other small Mach number asymptotic models are shown to be a very good and fast alternative to a fully compressible model. A numerical scheme is proposed and completed with numerical simulations. Being a compromise between highly sophisticated CFD simulations and basic empirical formulas this approach is appropriate to perform parameter studies or to apply parameter studies (e.g. diameter, height, heat loss etc.) or to apply control procedures.
Declarations
Authors’ Affiliations
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