CFD analysis of gas explosions vented through relief pipes
Introduction
Vent devices for gas and dust explosions are often ducted to safe locations by means of relief pipes, for the discharge of hot combustion products – even toxic – or blast waves [1], [2]. Relief pipes are specifically required when the hot jet flowing violently from the vent area has to be avoided, e.g. within buildings. On the other hand, the presence of a duct is likely to increase the severity of the explosion with respect to simply vented vessels [2], [3], [4], [5].
In the last two decades a number of works have addressed the issue of gas explosions vented through relief pipes [4], [5], [6], [7], [8], [9]. Several phenomena were identified as affecting the increase of the overpressure with respect to simply vented vessels such as secondary explosion in the duct (burn-up), frictional drag and inertia of the gas column in the duct, acoustic and Helmholtz oscillations.
Acoustic oscillations are deemed to be involved in the generation of later strong pressure peaks in simply vented vessels [10]. Kordylevski and Wach [7] detected acoustic oscillations in the pressure records of their experiments on small-scale ducted vent explosions suggesting this phenomenon could be somehow responsible for the unusual pressure rise in the vessel. Actually the link was quite loose as they observed stronger pressure rises (with respect to simply vented vessels) also in the absence of oscillatory behaviour. Moreover, Ponizy and Leyer [5] reported an increased violence of the duct-vented explosion on a small scale with stoichiometric propane–air mixtures which does not constitute a suitable condition for acoustic enhancement of explosion [11]. Helmholtz oscillations in small explosion chambers fitted to venting ducts were observed early by Cubbage and Marshall [12]. Also, McCann et al. [13] clearly detected Helmholtz oscillations in the final stages of explosions in small-scale vessels fitted to duct of different lengths. They pointed out that such oscillations could play an important role in triggering Taylor instability. Nevertheless, this effect cannot be considered necessary condition for the increase of the explosion violence, as the occurrence of this flame front instability is well acknowledged even in simply vented vessels [14]. Besides, as pointed out by the same authors, such oscillations should have more pronounced effects on larger scale explosions as confirmed by Kumar et al. [15], who detected severe Helmholtz type oscillations for middle scale lean hydrogen–air explosions vented through a duct.
The turbulent mixing of hot and fresh gases in the initial section of the duct after the flame entrance promotes a violent burning therein (an explosion-like combustion or “burn-up”). Hence, the pressure impulse in the duct induces the backflow of gases from the duct to the vessel with the possible consequent turbulization of residual combustion in the vessel and the blockage of the gas efflux [4], [5]. This violent explosion in the duct named as burn-up was addressed by some authors as the main responsible for the dramatic increase of the pressure in the vessel [4], [5], [9], [16].
Other authors indicated additional pressure drops due to the resistance of the gas flow in the vessel–duct assembly as main responsible for the higher pressure rise in the vessel with respect to simply vented vessels [17], [18]. Mechanical, steady-state type pressure drops for the present configuration can be substantial due to the very high flow velocities attained in the duct and the concentrated losses in the sudden flow area changes (respectively, at the duct entrance and exit).
On the theoretical side, some efforts have been devoted to get insights into the phenomenon by developing mathematical models. Zero-dimensional models proved effective in advancing the comprehension and the formalization of data gained for simply vented explosions [19], [20], [21]. Zero-dimensional and one-dimensional models [4], [17] were also proposed to represent an explosion vented through a duct but result in a scarce predictive capability as they rely strongly on empirical parameters. In fact, it could not be expected that such models provided a sound description of the phenomenon due to the assumption of a spherical flame propagation whatever the geometric complicacy (here included the presence of a discharging duct). According to these models the enhancement of the burning rate through turbulization [4] and the friction losses [17] are the most important phenomena affecting overpressure.
The available guidelines for the design of ducted vents for gas explosions are those proposed by Bartknecht [3], also reported in NFPA 68 [1], which gives barely an empirical correlation based on simply vented vessels indications presented in the same reference. Due to their empirical foundation, NFPA correlations are to be used very carefully as they can lead to gross errors [20].
Prior to any correlation development, a sensible approach should be trying to understand the relative contribution of all above reported events to the whole phenomenon. This step appears to be preparatory (if not mandatory) for the selection of the ruling parameters and for the making of the necessary approximations aiming at developing sound engineering correlations.
To this regard it must be noticed that, when care is used in analyzing their results, computational fluid dynamic (CFD) models can be valuable tools in assessing explosion scenarios provided that a satisfactory validation is carried out [22], [23], [24], [25], [26]. CFD models can in principle take into account much more physics than zero-dimensional models as they can, for example, relieve the severely restrictive hypothesis on the geometry of the system and of the propagating flame.
In this work a theoretical model for the gas explosion vented through a duct has been developed and numerically solved by means of the CFD-ACE+ code by CFDRC [27]. The model has been validated and tested against the comprehensive set of experimental data of Ponizy and Leyer [5], [9]. Comparison of model predictions with experimental data is presented and explanations of experimental observed trends are proposed on the basis of model results. More specifically, the effects of varying the duct geometry (length and diameter) and the ignition position have been studied and analysed with the aid of the numerical computations. Detailed field data gained from the calculations have allowed to evaluate selectively the relative contribution of the mechanical (hindered gas efflux) and chemical (enhanced combustion) contributions to the final pressure load recorded in the system.
Section snippets
The model
The analysis of ducted vented explosion has been performed by means of a finite-volume CFD two-dimensional (2D) axis-symmetric model based on the unsteady Reynolds Averaged Navier Stokes (RANS) approach.
Results and discussion
In the following, the model results are compared with the experimental results of Ponizy and Leyer [5], [9]. Hence, insights into the phenomena affecting the dramatic increase of pressure in the case of ducted venting are given.
A base case is first defined as the case with tube length Lt = 2.6 m and diameter Dt = 0.036 m and rear ignition.
For this configuration, Fig. 2 shows the pressure histories in the vessel (monitor 3 in Fig. 1) as obtained by the experiment [5] and by the numerical simulation.
Model performance evaluation
In order to verify the CFD model used we have applied the test based on MEGGE Protocol by European Community for gas explosion model evaluation [43]. According to this test, it is possible to evaluate the performance of the model by calculating the bias and the variance. We have then represented our model results in comparison with the experimental results of Ponizy and Leyer [5], [9] in the mean-variance diagram. The geometric mean (GM) and the variance (σ) have been calculated as follows:
Conclusions
A CFD model based on the unsteady RANS approach for the numerical simulation of a gas explosion vented through a duct has been proposed.
In this model an adjustable parameter is present for the calculation of the flame area of the laminar combustion rate. This parameter has been identified by matching the computed and the experimental pressure of the rear ignition case. The model has then been validated by comparing the simulation results with the experimental values of peak pressure and flame
References (43)
Explosion venting technology
J. Loss Prev. Process Ind.
(1996)- et al.
Flame dynamics in a vented vessel connected to a duct: 1. Mechanism of vessel–duct interaction
Combust. Flame
(1999) - et al.
Influence of ducting on explosion pressure: small scale experiments
Combust. Flame
(1988) - et al.
Flame dynamics in a vented vessel connected to a duct: 2. Influence of ignition site, membrane rupture, and turbulence
Combust. Flame
(1999) - et al.
On the role of acoustically driven flame instabilities in vented gas explosions and their elimination
Combust. Flame
(1983) - et al.
On the mechanisms of pressure generation in vented explosions
Combust. Flame
(1986) - et al.
Gasdynamics of vented explosions Part I: Experimental studies
Combust. Flame
(1985) - et al.
Observation of flame instabilities in large scale vented gas explosions
A simplified method for predicting the effect of ducts connected to explosion vents
J. Loss Prev. Process Ind.
(1993)- et al.
The effect of vent ducts on the reduced. explosion pressures of vented dust explosions
J. Loss Prev. Process Ind.
(1988)
Venting of deflagrations: hydrocarbon air and hydrogen–air systems
J. Loss Prev. Process Ind.
Vented gaseous deflagrations: modelling of hinged inertial covers
J. Hazard. Mater.
Numerical simulations of turbulent gas flames in tubes
J. Hazard. Mater.
Experimentally validated 3-D simulation of shock waves generated by dense explosives in confined complex geometries
J. Hazard. Mater.
Investigations to improve and assess the accuracy of computational fluid dynamic based explosion models
J. Hazard. Mater.
Solution adaptive CFD simulation of premixed flame propagation over various solid obstructions
J. Loss Prev. Process Ind.
The challenge of turbulent combustion
Turbulent combustion modeling
Prog. Energy Combust. Sci.
A turbulent reaction rate model for premixed turbulent combustion in spark-ignition engines
Combust. Flame
Premixed flame propagating into a narrow channel at a high speed, Part 1: flame behaviours in the channel
Combust. Flame
The venting of gaseous explosions in spherical vessels. I—theory
Combust. Flame
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