A shock-tube investigation of the dynamics of gas-particle mixtures: Implications for explosive volcanic eruptions

Authors


Abstract

[1] We use 1-D shock-tube experiments to investigate the dynamics of rapidly-decompressed gas-particle mixtures and associated shock waves, with application to the initial stages of Vulcanian and Plinian eruptions. For particle sizes 45–150 μm and pressure ratios 1–70, experimental particle Reynolds numbers reach 104 and impulsive accelerations reach 150 g. The experiments suggest that particles hinder gas motion via an interphase drag force, reducing shock strength and velocity. Gas-particle mixture velocities decrease with increasing particle diameter for a given initial pressure ratio and are less than those predicted by pseudogas approximations and existing interphase drag relationships due to imperfect phase coupling and unsteady flow during high-acceleration stages. We present a new analysis for predicting shock strength and velocity for gas-particle mixtures, and apply our improved interphase drag terms to the high-acceleration, eruption initiation stage of Vulcanian eruptions.

1. Introduction

[2] High-speed gas-particle flows result from explosive volcanic activity in the form of stratospheric scale Plinian eruptions, smaller scale Vulcanian explosions, and pyroclastic flows. In this paper, we use 1-D shock tube experiments [after Anilkumar et al., 1993; Cagnoli et al., 2002] to understand the behavior of rapidly-decompressed gas-particle mixtures and associated shock waves. Gas-particle mixtures from explosive volcanic flows are commonly approximated as a single, perfectly-coupled fluid, or pseudogas, whose bulk properties are described as simple functions of gas volume fraction [e.g., Wallis, 1969; Wilson et al., 1980; Kieffer, 1981; Melnik et al., 2005]. This approach is not realistic for all eruptive conditions, so interphase drag relationships have been used to account for slip between gas and particles [e.g., Valentine and Wolhetz, 1989; Dobran et al., 1993; Neri and Macedonio, 1996]. However, these are typically derived from steady-state experiments [e.g., Ergun, 1952], which seem to be inappropriate for high accelerations associated with eruption initiation. Understanding the dynamics of rapidly accelerating gas-particle mixtures and their interaction with shock waves is important for testing explosive eruption models, and for interpretation of microbarograph measurements of pressure waves at active volcanoes [Ishihara, 1985; Morrissey and Chouet, 1997; Johnson et al., 2003].

[3] After introducing shock-tube theory and describing our experimental methods (sections 2 and 3), we compare our laboratory results with existing pseudogas and interphase drag relationships (sections 4 and 5). We then present a new analysis of the behavior of rapidly decompressed gas-particle mixtures, yielding new interphase drag relationships, and discuss implications for shock wave characteristics and gas-particle mixture acceleration (section 5). We then apply our findings to typical Vulcanian eruptions (section 6).

2. Background

[4] The classical shock tube consists of a high-pressure gas (driver section) separated from a low-pressure gas (expansion section) by a diaphragm (Figure 1a; after Saad, 1985). Instantaneous rupture of the diaphragm forms a normal shock wave that travels at supersonic speed through the expansion section, while rarefaction waves travel into the driver section at the sound speed of the driver gas [Saad, 1985]. The initial pressures in the driver and expansion sections are p4 and p1, respectively, and the pressure behind the shock is p2. The shock strength equation image for inviscid flow is

equation image

where Ms is the shock Mach number (the ratio of the shock speed to the sound speed, c, of the expansion section gas), and γ is the ratio of specific heats for the gas, (Figure 1a and 1b). The gas velocity behind the shock is [Saad, 1985]

equation image
Figure 1.

Shock tube schematics.

3. Experimental Method

[5] In 1-D shock tube experiments, monodisperse mixtures of Ballotini glass spheres (Potters Inc.) and interstitial air were rapidly decompressed. The spheres were loaded into the high-pressure test section at atmospheric pressure (Figure 1c), with gas volume fractions α between 0.40–0.47. A plastic diaphragm was placed between the driver and expansion sections, and the expansion section was pumped down to vacuum pressures. A Redlake high-speed video camera (250–500 fps) and piezo-electric pressure sensors (PCB Inc., sampling at 100 kHz) were triggered simultaneously with diaphragm rupture, to measure mixture and shock velocities. The pressure ratio across the diaphragm p4/p1 was varied from 1–70 for each of three particle sizes 45, 90 and 150 μm. Further experiments with small (4 cm) and large (12 cm) gaps between the diaphragm and the top of a bed of 45 μm particles were performed to determine the sensitivity of the flow dynamics to gap spacing. Shock strength was calculated directly as the ratio of pressures on either side of the shock (identified in the pressure transducer data as a sharp, significant increase in pressure). Shock velocities were determined using the known distance between pressure sensors (32 cm) and the difference in the arrival times of the shock at each sensor. High-speed videography was used to track the mixture flow front. As observed by Cagnoli et al. [2002], some of the flow fronts were irregular adding a small unsystematic error to the mixture velocity.

4. Experimental Results

[6] Figure 2 shows the relationship between p4/p1 and the velocity (Figure 2a) and strength (Figure 2b) of the shock generated by the decompression experiments. The shock strengths and velocities in the experiments with air only (no particles) on both sides of the diaphragm (open triangles) generally agree with values predicted by 1-D shock tube theory (solid line; equation (1)) for air at a sound speed of 330 m s−1, appropriate for our laboratory conditions.

Figure 2.

(a) Shock velocity and (b) strength data vs. pressure ratio across the diaphragm (p4/p1) for experiments with only air as the driver and expansion gases (open triangles), and experiments with 45 (solid squares), 90 (dots), and 150 μm (open circles) particles. The error for all experimental data is the radius of the plotted symbols. Also shown are 1-D shocktube theory for an ideal gas (solid line), the pseudogas approximation from Dobran et al. [1993] (dotted dashed line), and our new model incorporating interphase drag (equations (4) to (7); dashed line).

[7] The presence of particles in the experiments (squares, dots, open circles) reduces shock velocities by approximately 30–40% and strengths by almost 60% compared to the air experiments. There is no obvious correlation between particle size and shock velocity or strength, with all particle-size data forming a single trend. A gap of ≥4 cm between the diaphragm and the top of the particle bed produces shock velocities similar to experiments with air only, suggesting that shock properties are not sensitive to the gap size. For comparison (Figure 2; dotted dashed line), a pseudogas approximation [Dobran et al., 1993, equations (40) and (41)] underestimates shock velocities and strengths for experiments with particles, where α = 0.4, c4 = 13 m s−1, and γ4 approaches 1 [Wohletz, 2001].

[8] Maximum gas-particle mixture velocities occurred in the first 1–12 ms of the experiments, corresponding to accelerations up to 150 g. Mixture velocities increase with increasing pressure ratio and generally decrease with increasing particle size for a given pressure ratio (Figure 3). 1-D shock tube theory using air as an ideal gas significantly overpredicts the mixture velocity and is not plotted. Cagnoli et al. [2002] found that a pseudogas approximation is reasonable for mixture velocities with pressure ratios <10 and particle sizes <38 μm. However, our expanded data set shows the pseudogas approximation (Figure 3; dotted dashed line) overpredicts mixture velocities at higher pressure ratios and for larger particles.

Figure 3.

Mixture velocity vs. pressure ratio across the diaphragm (p4/p1) for experiments with 45 (solid squares), 90 (dots), and 150 μm (open circles) particles. Error for all experiments is the radius of the plotted symbols. Also shown are the pseudogas approximation of Dobran et al. [1993] (dotted dashed line), predictions of the first term of the Ergun [1952] equation with 90 μm particles (dashed line), and our new model for 45 μm (solid line) and 150 μm (dotted line) particles.

5. Interpretation of Results

[9] The initial state of our experiments consists of a packed bed of particles and interstitial air at atmospheric pressure. Upon decompression, the interstitial air rapidly expands, generating a shock wave which propagates faster than the subsequent motion of the air-particle mixture (Figure 1d). Shock strength and velocity are reduced compared to experiments with air only, suggesting that significant drag forces are generated on the air when the expanding gas initially propagates through interstices in the particle bed. A pseudogas approximation underpredicts the shock strength and velocity (Figure 2; dotted dashed line) because experimental observations suggest the shock wave is formed by air, not by an air-particle mixture. Subsequently, the drag of the air generates particle motion. Our experimental results show the velocity of the gas-particle mixture is less than that predicted by pseudogas approximations due to imperfect coupling between particles and air, as has been proposed for large pressure ratios [Cagnoli et al., 2002].

[10] We now estimate the magnitude of the interphase drag forces using two methods. First, we calculate the drag force exerted by the particles on the air by examining air motion across the shock wave, and then we quantify the drag force exerted by the air on the particles by examining the motion of the air-particle mixture.

5.1. Modified Shock Relationship

[11] The drag force exerted by the particles on the expanding air can be introduced into the momentum equation for a control volume (CV1) across the shock wave (Figure 1d) as follows

equation image

where Fda is the drag force exerted by the particles on the air and A is the cross sectional area of the shock tube occupied by the air (αAtube, where Atube is the cross-sectional area of the test section), and subscripts 1 and 2 refer to properties of the air in front of and behind the shock, respectively (equation (1); Figure 1; modified from Saad, 1985). Equation (3) balances the vertical forces acting on the air in the CV, the net pressure force (first two terms on LHS) and the drag force exerted by the particles (third term on LHS), against the net momentum change across the CV, the difference between momentum entering and leaving the CV (terms on RHS). Rearranging and using the continuity equation for constant A and standard relationships for compressible flow, the modified shock strength can be written as

equation image

[12] Thus, the shock strength formed by gas-particle mixtures is simply that predicted for inviscid flow of an ideal gas alone (equation (1)) reduced by the factor equation image. In conventional form

equation image

where Cd is only a function of particle Reynolds number, NRe. Generally, Cd = k1(NRe)β for 0.1 < NRe < 105, where values of β for single spheres and beds of spheres fall between 0 and −1.3 [Figure 4; Batchelor, 1967; Ergun, 1952]. Rewriting the drag term in equation (4)

equation image

where NRe = (ρ2u2dp)/μ2, dp is particle diameter, p1 = ρ1RT (ideal gas), and k2 is a coefficient that incorporates the remaining terms. The density ratio across the shock for a calorically perfect gas is

equation image

[Saad, 1985]. The trend in our shock data is most closely matched when k2 = 7.7 × 10−3 and β = −1.2 (Figure 2; dashed line). A narrow range of acceptable β values falls between −1.25 and −0.9.

5.2. Interphase Drag Relationships

[13] For a second CV bounded at the bottom by the diaphragm and at the top by the point of maximum mixture velocity (∼20 cm above the diaphragm; Figure 1d, CV2), the momentum equation in the vertical direction for the gas-particle mixture is given by

equation image

where Fdp is the drag force the air exerts on the particles, t is time, V is volume, CS is the control surface perpendicular to the vertical axis and umix is the measured mixture velocity. In this form, the momentum equation describes the drag, gravity and pressure forces (terms on LHS) that generate the net momentum change of the mixture across the CV (terms on RHS). We solved equation (8) for Fdp and calculated the total drag force of the air on the particles for each experiment. We then used a conventional expression for Fdp (e.g., equation (5)) to calculate corresponding Cd's, leading to the following relationship (Figure 4)

equation image
Figure 4.

Interphase Cd vs. NRe for experiments with 45 (solid squares), 90 (dots), and 150 μm (open circles) particles. The interphase Cd suggested by Ergun [1952] for steady flow of air through stationary packed particle beds (90 μm particles; open triangles).

[14] The interphase drag force is controlled by the velocity difference between particles and gas. Because this velocity difference is dominated by air velocity during initial acceleration, u2 (equation (2)) calculated from the reduced shock strength (equation (4)) is used in NRe. Equation (9) follows the functional form for single spheres and beds of spheres identified earlier in the shock analysis, consistent with theory [Batchelor, 1967; Ergun, 1952]. However, for our experiments (102 < NRe < 104), k1 = 7 × 104 and β = −0.9 (Figure 4), values which are inconsistent with constants previously obtained for steady-state experiments [Ergun, 1952]. According to our experiments, reasonable values of β fall between −1.2 and −0.70, consistent with values obtained from shock observations (section 5.1). Different values of the pre-multiplying constants obtained in the mixture and shock analyses reflect the different stages of particle motion and gas expansion in each case.

[15] The interphase drag relationship suggested by Ergun [1952] for steady flow of air through stationary packed particle beds for NRe < 10 (first of two terms) can be rewritten as a drag coefficient as follows

equation image

for our experimental conditions. This relationship overpredicts the values of the experimentally determined Cd's by a factor of ∼2.5, but the trend parallels our own. The trend for 90 μm particles (open triangles) is shown in Figure 4 for comparison. Use of the Ergun term for NRe > 10 significantly overpredicts our experimental Cd's and is not plotted.

6. Implications for Eruption Dynamics

[16] The gas-particle mixture velocity at the vent is a critical parameter that determines whether pyroclastic flows will subsequently develop [Sparks et al., 1978; Wilson et al., 1980]. Thus, a method of predicting initial explosion velocity for a given conduit pressure is valuable. Conversely, accurately describing the relationship between conduit pressure and explosion velocity and shock wave characteristics provides an estimate of pre-eruption conduit pressures from field observations.

[17] Shallow conduit overpressures on the order of 5–10 MPa precede Vulcanian eruptions, corresponding to initial pressure ratios of 50–100 [Stix et al., 1997; Voight et al., 1999]. For initial α = 0.4 and pressures in this range, our experimental data suggest that instantaneous decompression generates mixture velocities of 15–40 m s−1, whereas a pseudogas approximation predicts velocities up to four times greater, and the drag coefficient as described by Ergun [1952] predicts mixture velocities up to two times greater. We expect higher experimental mixture velocities for α > 0.4 for the same pressure range.

[18] Six Vulcanian eruptions during 1982–1983 at Sakurajima volcano, Japan, had explosion (mixture) velocities of 21–33 m s−1 and shock velocities of 440–500 m s−1 [Ishihara, 1985]. Our analysis of these explosion velocities suggests pre-eruption conduit pressures of 1.5–10 MPa, compared to conduit pressures of 0.4–1.2 MPa estimated using pseudogas theory. Similarly, Vulcanian eruptions during 2002–2004 at Santiaguito volcano, Guatemala, had explosion velocities of 5–30 ms−1 [Bluth and Rose, 2004] with our theory suggesting initial pressure ratios of 5–100. Our analysis of Sakurajima shock velocities produces conduit pressures of 4–7.5 MPa consistent with the mixture velocity estimates, whereas assuming inviscid flow of an ideal gas suggests conduit pressures of 0.6–1.0 MPa. Given overpressures typically associated with Vulcanian eruptions (5–10 MPa) and the rupture strength of many volcanic rocks (>4 MPa [Stix et al., 1997; Voight et al., 1999]), pseudogas and inviscid shock theories appear to significantly underestimate pre-eruption conduit pressures.

7. Conclusions

[19] Shock strength and velocity are reduced for rapid decompression of solid-gas mixtures as compared to decompression of an ideal gas alone (102 < NRe < 104; 1 < p4/p1 < 70). The magnitude of the reduction is independent of particle size and can be expressed as a simple function of gas properties (equation (6)). Pseudogas theory underpredicts both the shock strength and velocity, and overpredicts maximum gas-particle mixture velocities, which decrease with increasing particle diameter for a given initial pressure ratio. Expressions used previously to describe drag between gas and particles do not correctly predict the maximum mixture velocities observed in our experiments. We therefore present new predictions for shock strength and velocity for gas-particle mixtures (equations (4) to (7)), which are in accord with experimental observations, and develop an improved interphase drag relationship for the eruption initiation stage (equation (9)).

Acknowledgments

[20] This research was supported by the Royal Society of London and NSF EAR0541925. Insightful comments from an anonymous reviewer improved the manuscript.

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