Mathematical Problems in Engineering

Mathematical Problems in Engineering / 2011 / Article

Research Article | Open Access

Volume 2011 |Article ID 536056 | 14 pages | https://doi.org/10.1155/2011/536056

On the Critical Behaviour of Exothermic Explosions in Class A Geometries

Academic Editor: J. Jiang
Received30 Mar 2011
Accepted16 Jun 2011
Published09 Aug 2011

Abstract

The aim of this work is to apply the homotopy perturbation method for solving the steady state equations of the exothermic decomposition of a combustible material obeying Arrhenius, Bimolecular, and Sensitised laws of reaction rates. These equations are formulated on some Class A geometries (an infinite cylinder, an infinite slab, and a sphere). We also investigate the effect of Frank-Kamenetskii parameter on bifurcation and thermal criticality by means of the Domb-Sykes graphical method.

1. Introduction

The safety in transport and storage of combustible materials is a key issue in pyrotechnic applications. These materials are often subjected to self-ignition. This internal heating occurs when an explosive substance is brought to a sufficient temperature so that the process of decomposition begins to produce significant exothermic effects. This involves a thermal runaway phenomenon accompanied with an increase of the temperature producing a rapid thermal decomposition. The understanding of the factors that control this phenomenon is of fundamental importance in many industrial processes.

This phenomenon was first introduced in the 1930s by Semonov, Zeldovith and Frank-Kamenetskii, and their pioneering contributions were summarized in [1]. Furthermore, Frank-Kamenetskii developed the steady-state theory of thermal explosion. In this theory, the Frank-Kamenetskii approximation allows us to determine the critical values, which constitute limit values not to be exceeded to avoid the phenomenon of self-ignition. Some studies deal with a chain of several reactions in this phenomenon of self-ignition. Several works in the literature have applied this theory to different combustible materials geometries. Boddington et al. [2–4] have considered the special case of two-step parallel exothermic reactions for the infinite slab where solutions by quadrature were possible. Graham-Eagle and Wake [5] considered a system of simultaneous exothermic reactions. They extended the investigations of Boddington et al. [2–4] to the other two geometries of the infinite circular cylinder and the sphere. A variational method was used to evaluate the critical values of Frank-Kamenetskii parameter and the maximum temperature. The same authors [6] extended the treatment of simultaneous reactions to the case where one reaction is exothermic and the other endothermic, leading to the phenomenon of the disappearance of criticality or transition, which can also happen with a single reaction in the case of very low activation energy. In this case, the Frank-Kamenetskii approximation is no longer valid. They used a variational method [7] to determine numerically the values of the parameter which characterizes the transition in the parameter space.

Recently, Ajadi and Gol’dshtein [8] employed a three-step reaction kinetics model (initiation, propagation, and termination steps). The calculation of the criticality was made by means of a variational method for (infinite slab, infinite cylinder, and sphere) under Arrhenius laws of reaction rates by using an effective activation energy approximation. Balakrishnan et al. [9] calculated the critical values for some non-Class A geometries (infinite square rod and cube). Their critical values were found using the finite difference method.

In applied mathematics or engineering problems, numerical methods commonly used such as finite difference, finite element, or characteristics method, need large size of computational works due to discretization and usually the effect of round-off error causes loss of accuracy in the results. In addition to this drawback, these methods with limited precision include slow runtimes, numerical instabilities, and difficulties in handling redundant constraints.

Analytical traditional methods commonly used for solving these problems can be very useful, especially for the calibration of numerical calculations. Among these approaches, the classical perturbation method is based on the existence of small parameters but the overwhelming majority of linear and nonlinear problems have no small parameters, at all.

To overcome this shortcoming, the homotopy perturbation method (HPM) was first introduced by He [10–13]. The main idea of this method is to introduce an embedding parameter 𝑝∈[0,1] to construct a homotopy and give solutions of the deformed problem as power series in 𝑝. When 𝑝=0, the system of equations is reduced to a simplified form which admits exact solutions, and, at 𝑝=1, the system takes its original form and gives the desired solutions. This method has been extensively employed by numerous authors to solve a large variety of linear and nonlinear problems. We can cite the works [14–17], the list is not exhaustive.

In this paper, we examine the steady-state solutions for the strongly exothermic decomposition of a combustible material of a symmetric Class A geometries, uniformly heating, under Arrhenius, Biomolecular, and Sensitised kinetics, neglecting the consumption of the material.

The contribution of the present work is twofold. First, we calculate the temperature field using the HPM in a symbolic computational language. The second aim is to study the thermal criticality conditions of the problem.

Critical values for different geometries are found by using the Domb-Sykes technique [18] as a useful tool to extract singularities and to perform analytic continuation. This method has shown to be very accurate and simpler to implement, when compared with variational method [6, 8] or Hermite-Padé approximants method [19–21].

The structure of this paper is as follows. Section 2 presents the boundary value problem governing the ignition of a viscous combustible material for symmetric Class A geometries. In Section 3, we will apply the homotopy perturbation method to this nonlinear boundary value problem. The fourth section is assigned to a brief description of the Domb and Sykes method and its application to calculate the bifurcation points. Section 5 is devoted to the results obtained by the proposed method, and comparison with other works will be performed. Conclusions will appear in Section 6.

2. Mathematical Model

We consider the steady-state solutions for the strongly exothermic decomposition of a viscous combustible material. Neglecting the reactant consumption, the equation for the temperature 𝑇(𝑟) may be written in terms of physical variables together with the boundary conditions as follow:𝑑2𝑇𝑑𝑟2+𝑗𝑟𝑑𝑇+𝑑𝑟𝑄𝐶0ğ´ğ‘˜î‚€ğ¾ğ‘‡î‚ğœâ„Žğ‘šğ‘’âˆ’ğ¸/𝑅𝑇=0,(2.1)𝑑𝑇𝑑𝑟(0)=0,𝑇(ğ‘Ž)=𝑇0,(2.2) with 𝑇 the absolute temperature, 𝑇0 the wall temperature, 𝑘 the thermal conductivity of the material, 𝑄 the heat of reaction, 𝐴 the rate constant, 𝐸 the activation energy, 𝑅 the universal gas constant, 𝐶0 the initial concentration of the reactant species, ℎ the Planck’s number, 𝐾 the Boltzmann’s constant, 𝜐  the  vibration frequency, ğ‘Ž the geometry half width, and 𝑟 the radial distance in the normal direction. 𝑚 is the numerical exponent, such that 𝑚=−2,0,1/2 represent numerical exponent for Sensitised Arrhenius and Bimolecular kinetics (Boddington et al. [3], Makinde [20], Bowes [22], Bebernes and Eberly [23], Okoya [24]), and 𝑗=0,1,2 is the geometry factor representing, respectively, slab, cylindrical, and spherical geometries.

The following dimensionless variables and parameters are introduced in (2.1):𝐸𝜃=𝑇−𝑇0𝑅𝑇20,𝑟𝑟=ğ‘Ž,𝜀=𝑅𝑇0𝐸,𝛿=ğ‘„ğ¸ğ´ğ‘Ž2𝐶0𝐾𝑚𝑇0𝑚−2ğœğ‘šâ„Žğ‘šğ‘’ğ‘…ğ‘˜âˆ’ğ¸/𝑅𝑇0,(2.3) to obtain the dimensionless governing equation together with the corresponding boundary conditions. We get the following equations:𝑑2𝜃𝑑𝑟2+𝑗𝑟𝑑𝜃𝑑𝑟+𝛿(1+𝜀𝜃)𝑚𝜃exp1+𝜀𝜃=0,(2.4)𝑑𝜃𝑑𝑟(0)=0,𝜃(1)=0,(2.5) where 𝛿, 𝜀 represent the Frank-Kamenetskii and activation energy parameters, respectively. Hereafter, we will suppress the bar symbol for clarity.

3. Homotopy Perturbation Method Solution

In this section, we will apply the homotopy perturbation method (HPM) to nonlinear ordinary differential equation (2.4). According to this method, we can construct a homotopy as follows:𝑑(1−𝑝)L(𝜙)+𝑝2𝜙𝑑𝑟2+𝑗𝑟𝑑𝜙𝑑𝑟+𝛿(1+𝜀𝜙)𝑚𝜙exp1+𝜀𝜙=0,(3.1) where 𝑑L(𝜙)=2𝜙𝑑𝑟2+𝑗𝑟𝑑𝜙𝑑𝑟.(3.2) Applying the perturbation technique [25], we can assume that the solution of (3.1) can be expressed as a series in 𝑝𝜙(𝑟,𝑝)=𝑓0(𝑟)+𝑝𝑓1(𝑟)+𝑝2𝑓2(𝑟)+⋯,(3.3) where 𝑝∈[0,1] is an embedding parameter. When 𝑝=0, we can obtain the initial guesses; when 𝑝=1, (3.1) turns out to be the original one.

Setting 𝑝=1, we obtain an approximate solution of (2.4):𝜃=lim𝑝→1𝜙(𝑟,𝑝)=𝑓0(𝑟)+𝑓1(𝑟)+𝑓2(𝑟)+⋯.(3.4) One has to substitute relation (3.3) into the governing equation (3.1), collect the powers of 𝑝, and obtain a sequence of differential equations and boundary conditions. The solution for the temperature field for Sensitised, Arrhenius, and Bimolecular reaction rates for different geometries are given as1𝜙(𝑟,𝑝,𝑗=0)=−2𝑟𝑝𝛿2+1−1𝑝242𝛿2𝑟2𝑟−12𝑝−5(𝑚𝜀+1)+𝑂3,1𝜙(𝑟,𝑝,𝑗=1)=−4𝑟𝑝𝛿2+1−1𝑝642𝛿2𝑟2𝑟−12𝑝−3(𝑚𝜀+1)+𝑂3,1𝜙(𝑟,𝑝,𝑗=2)=−6𝑟𝑝𝛿2+1−1𝑝3602𝛿2𝑟2−13𝑟2𝑝−7(𝑚𝜀+1)+𝑂3.(3.5) According to (3.4), we get the solution for the temperature field for the three reaction rates.

4. Bifurcation Study by Domb-Sykes Method

The modelling of physical phenomena often results in nonlinear problems for some unknown function, say 𝑓(𝜆) depending on a parameter 𝜆. Usually, the problems cannot be solved exactly. The solutions of these nonlinear systems are dominated by their singularities which must be real and positive in order to have a physical sense.

We suppose that up to the point 𝜆0, the solution is analytic in the interval ]−𝜆0,𝜆0[, then one can solve the problem by expanding the solution in a power series𝑓(𝜆)=âˆžî“ğ‘›=0𝑐𝑛𝜆𝑛.(4.1) If an infinite number of 𝑐𝑛 is known, the radius of convergence, which is the distance from the origin to the nearest singularity, limiting the range of validity of the series (4.1), can be calculated using D’Alembert’s ratio.

However, for most nonlinear problems, it is rare to find an unlimited number of terms of the power series (4.1). The nearest singularity cannot therefore be determined precisely.

Using symbolic calculus codes, it is now possible to calculate a sufficient number of terms in the series, to study precisely the solution, and there exist a variety of methods devised for extracting the required information of the singularities from a finite number of series coefficients. The most frequently used methods are the ratio-like methods, such as the Domb-Sykes method [26, 27], Neville-Aitken extrapolation [26], and seminumerical approximant methods, such as Padé approximants [28] or Hermite-Padé approximants [19–21].

Herein, we are concerned with the bifurcation analysis by analytic continuation as well as with the dominant behavior of the solution by using partial sum (3.3). This may be done calculating the nearest singularity to the origin. A useful tool for extracting this singularity is the Domb-Sykes method. This technique is easier to implement than others, and, when it is improved, it gives a precise value of the singularity. This method, successfully applied in various problems [29–32], is presented here.

According to Fuchs (Bender and Orszag [27]), there are two possible forms:𝑓(𝜆)=âˆžî“ğ‘›=0𝑐𝑛𝜆𝑛=âŽ§âŽªâŽ¨âŽªâŽ©ğ›¼î€·ğœ†0−𝜆𝛾𝛼𝜆for𝛾≠0,1,…,𝑛,…,0−𝜆𝛾𝜆ln0−𝜆for𝛾=0,1,…,𝑛,….(4.2) The radius of convergence 𝜆0 of the series (4.1) may be found by d’Alembert ratio:𝜆0=limğ‘›â†’âˆž||||𝑐𝑛−1𝑐𝑛||||.(4.3) Of course, only a finite number of coefficients 𝑐𝑛 are known, so that it is difficult to obtain precisely the limit. Domb and Sykes have suggested that the inverse ratio |𝑐𝑛/𝑐𝑛−1| has the following expansion:ğ‘Žğ‘›=||||𝑐𝑛𝑐𝑛−1||||=1𝜆01−1+𝛾𝑛1+𝑜𝑛1=â„Žğ‘›î‚.(4.4) Domb and Sykes have pointed out that it is more reliable to plot |𝑐𝑛/𝑐𝑛−1| versus 1/𝑛, that is, to bring ğ‘›â†’âˆž to the origin, rather than plotting |𝑐𝑛−1/𝑐𝑛| versus 𝑛. The plot of |𝑐𝑛/𝑐𝑛−1| versus 1/𝑛 is known as Domb-Sykes plot. In this plot, the intersection of the straight line ğ‘Žğ‘›=ℎ(1/𝑛) with the axis 1/𝑛=0 is exactly 1/𝜆0, and the slope of this line gives the exponent 𝛾. Unfortunately, ğ‘Žğ‘› is often a slowly converging series. A good way to improve the convergence is to use the Richardson extrapolation (Bender and Orszag [27]), which is appropriate for this kind of sequences and can be defined as follows.

If ğ‘Žğ‘› can be written in the following form: ğ‘Žğ‘›=𝑆0+(𝑆1/𝑛)+(𝑆2/𝑛2)+⋯, then the Richardson extrapolation is𝑠𝑚𝑛=𝑚𝑘=0(−1)𝑘+ğ‘šğ‘Žğ‘›+𝑘(𝑛+𝑘)𝑚𝑘!(𝑚−𝑘)!.(4.5) This new sequence has a quicker convergence to the limit 𝑆0.

5. Results and Discussion

Using a computer algebra system, we obtained the first 30 terms of the solutions series (3.5).

In order to verify numerically whether the proposed methodology leads to high accuracy, we evaluate the numerical solutions using a collocation method proposed by Shampine et al. [33].

In Figures 1, 2, and 3, we have plotted the numerical and the HPM solutions in all Class A geometries and for all numerical exponent 𝑚. These figures show a perfect agreement of both solutions.

The obtained solutions, in comparison with the numerical solutions, admit a remarkable accuracy. A clear conclusion can be drawn from the numerical results that the HPM provides highly accurate numerical solutions for nonlinear differential equations.

For a further information, Figure 4 illustrates a comparison between the exact solutions known for the special cases (𝑚=0,𝜀=0,𝑗=0,𝑗=1) when a closed form is available [8] and the series solutions obtained by using the homotopy perturbation method. The obtained results are found to be in good agreement with the exact solutions. We can notice that the deviation between HPM and exact solution do not exceed 0.2% for both slab and cylindrical geometries.

In the following, we will focus on the calculation of radius of convergence 𝛿cr of the series solutions (3.5). Up to the point 𝛿𝑐, the solution 𝜃 is analytic and has a real singularity at the value 𝛿cr. It would be interesting to know the exact nature of the singularity and if this singularity corresponds to a bifurcation point. Let the maximum temperature 𝜃max=𝜃(0,𝛿,𝜀) be a characteristic quantity which qualifies the solution. We rearrange 𝜃max in a series of 𝛿 to write𝜃max=30𝑛=0𝑐𝑛(𝜀)𝛿𝑛,(5.1) where different coefficient 𝑐𝑛 for 𝜀=0 are given in Table 1. Seeing Figure 5, one can say that the ratio ğ‘Žğ‘›=|𝑐𝑛/𝑐𝑛−1| in the simple geometry of infinite circular cylinder converges; however, it is extremely difficult to conclude to a precise value of radius of convergence. It is necessary to use some process of convergence acceleration. The Richardson extrapolation is appropriate for this kind of convergence. The results of Table 2 show that the radius of convergence is 𝛿cr=2.  Two solution branches are therefore identified with a bifurcation point at 𝛿cr.  Two solution branches (type I and II) are identified with a bifurcation point at 𝛿cr (i.e., turning point) as shown in a sketch of bifurcation diagram in Figure 6.


n 𝑐 𝑛 𝑛 𝑐 𝑛 𝑛 𝑐 𝑛 𝑛 𝑐 𝑛 𝑛 𝑐 𝑛

10.2572.337 𝑒 − 4 131.455 𝑒 − 6 191.290 𝑒 − 8 251.338 𝑒 − 1 0
24.687 𝑒 − 2 89.588 𝑒 − 5 146.515 𝑒 − 7 205.978 𝑒 − 9 266.310 𝑒 − 1 1
31.302 𝑒 − 2 94.024 𝑒 − 5 152.939 𝑒 − 7 212.778 𝑒 − 9 272.982 𝑒 − 1 1
44.272 𝑒 − 3 101.720 𝑒 − 5 161.334 𝑒 − 7 221.296 𝑒 − 9 281.412 𝑒 − 1 1
51.538 𝑒 − 3 117.465 𝑒 − 6 176.096 𝑒 − 8 236.064 𝑒 − 1 0 296.700 𝑒 − 1 2
65.874 𝑒 − 4 123.279 𝑒 − 6 182.798 𝑒 − 8 242.845 𝑒 − 1 0 303.184 𝑒 − 1 2


n 𝑚 = 1 𝑚 = 2 𝑚 = 3 𝑚 = 4

200.49940.49990.50.4999
210.49940.50.49990.5
220.49950.50.50.4999
230.49950.50.49990.5
240.49950.49990.50.4999
250.49960.50.49990.5

It is possible to calculate the limited series defining 𝜃max=𝜃max(𝛿) by a division procedure. This function is plotted in Figure 7.

The graph of 𝜃max, as shown in Figure 6(a), is not compatible with the expected singularity (4.2). The curve 𝜃max versus 𝜃  should be in the form of Figure 6(b). To analyse the paradox, the inverse function 𝛿=𝛿(𝜃max) is considered. Its series is given by inverting the series 𝜃max. One can see in Figure 7 that this function has a horizontal tangent for the values in the case 𝑗=1, (𝜃max=1.38435,𝛿=1.99984).

We summarize the results of all Class A geometries in Tables 3, 4, and 5, while 𝜃cr=𝜃(0,𝛿cr,𝜀) is calculated by improving the series (5.1) by a suitable Padé approximant [27].


𝑗 𝛿 c r 𝛾 c r 𝜃 c r

00.878460.51.18684
120.51.38629
23.323240.51.61782


Exact methodVariational methodHermite-Padé approachPresent work

Slab 𝛿 c r = 0 . 8 7 8 4 6
𝜃 c r = 1 . 1 8 6
𝛿 c r = 0 . 8 7 8 3 5 5
𝜃 c r = 1 . 1 6 7 1 6
𝛿 c r = 0 . 8 7 8 4 5
𝜃 c r = 1 . 1 8 6 8 4
𝛿 c r = 0 . 8 7 8 4 6
𝜃 c r = 1 . 1 8 6 8 4

Cylinder —
—
𝛿 c r = 1 . 9 9 9 9 8
𝜃 c r = 1 . 3 8 0 1 1 9 7
𝛿 c r = 2
𝜃 c r = 1 . 3 8 6 2 9
𝛿 c r = 2
𝜃 c r = 1 . 3 8 6 2 8

Sphere—
—
𝛿 c r = 3 . 3 2 1 9 9
𝜃 c r = 1 . 6 0 7 4 6
—
—
𝛿 c r = 3 . 3 2 3 2 4
𝜃 c r = 1 . 6 1 7 8 2


𝑚 𝜀 𝛿 c r 𝜃 c r

−20.010.906241.24566
0.11.313892.22239

00.010.88781.19841
0.10.988191.52434

0.50.010.883311.19541
0.10.932211.42024

The critical values (𝛿cr and 𝜃cr) were computed using the improved Domb-Sykes applied to the temperature field obtained by HPM in all Class A geometries.

In order to verify the accuracy of this approximate method, we compare the critical values obtained using this method with the exact methods [1, 2], variational methods [5, 8], and Hermite-Padé approach [19–21] for the special case of 𝜀=0. The method used in the present work gives results approximately equal to those discussed in the literature, as shown in Table 4.

Tables 5, 6, and 7 depict the variations of 𝛿cr and 𝜃cr with 𝜀. In these tables, we observe that the magnitude of thermal criticality conditions for a viscous combustible material with high activation energy (𝜀=0) is lower than the one for moderate values of activation energy (𝜀=0.01, 𝜀=0.1). This implies that for moderate values of activation energy, the criticality varies from one reaction to another, as shown in Tables 5, 6, and 7. Explosion in Bimolecular reactions seems to occur faster than in Arrhenius and Sensitised reactions.


𝑚 𝜀 𝛿 c r 𝜃 c r

−20.012.064151.58738
0.13.016202.65419

00.012.022161.45337
0.12.261291.80247

0.50.012.011921.41353
0.12.132191.677327


𝑚 𝜀 𝛿 c r 𝜃 c r

−20.013.456411.67123
0.14.328712.1177

00.013.421121.62756
0.14.222452.21856

0.50.013.151671.63331
0.14.045672.23811

6. Conclusion

We studied the problem of exothermic explosion of a viscous combustible in Class A geometries under Arrhenius, Bimolecular, and Sensitised laws of reaction rates with the homotopy perturbation method. The results show that this method provides excellent approximation of the solution of this nonlinear system with high accuracy.

A bifurcation study is performed with the Domb-Sykes graphical method to calculate the critical value of this problem. The results show that these critical values increase with the activation energy.

Nomenclature

ğ‘Žâˆ¶Geometry half width
𝐴∶Rate constant
𝐶0∶Initial concentration of the reactant
𝐸∶Activation energy
ℎ∶Planck’s number
𝑗∶Geometry factor
𝑘∶Thermal conductivity of the material
𝐾∶Boltzmann’s constant
L∶Linear operator
𝑚∶Numerical exponent
𝑝∶Embedding parameter
𝑟∶Radial distance
𝑟∶Dimensionless radial distance
𝑄∶Heat of reaction
𝑅∶Universal gas constant
𝑇∶Absolute temperature
𝑇0∶Wall temperature.

Greek Symbols

𝜐∶Vibration frequency
𝜃∶Dimensionless temperature
𝜀∶Dimensionless activation energy
𝛿∶Frank-Kamenetskii parameter
𝛾∶Exponent.

Subscripts

cr:Critical
max:Maximum.

Acknowledgments

This work is supported by the French Ministry of Research and Education through invited professor contract. The authors are highly grateful to “ENSI de Bourges” for providing excellent research environment and facilities and to Professor J. H. He for his valuable comments.

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Copyright © 2011 Mustapha Er-Riani and Khaled Chetehouna. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

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