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<article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="1.3" xml:lang="en" article-type="research-article"><?properties manuscript?><processing-meta base-tagset="archiving" mathml-version="3.0" table-model="xhtml" tagset-family="jats"><restricted-by>pmc</restricted-by></processing-meta><front><journal-meta><journal-id journal-id-type="nlm-journal-id">9886760</journal-id><journal-id journal-id-type="pubmed-jr-id">22903</journal-id><journal-id journal-id-type="nlm-ta">Aerosol Sci Technol</journal-id><journal-id journal-id-type="iso-abbrev">Aerosol Sci Technol</journal-id><journal-title-group><journal-title>Aerosol science and technology : the journal of the American Association for Aerosol Research</journal-title></journal-title-group><issn pub-type="ppub">0278-6826</issn></journal-meta><article-meta><article-id pub-id-type="pmid">40160717</article-id><article-id pub-id-type="pmc">11951305</article-id><article-id pub-id-type="doi">10.1080/02786826.2024.2417976</article-id><article-id pub-id-type="manuscript">HHSPA2061031</article-id><article-categories><subj-group subj-group-type="heading"><subject>Article</subject></subj-group></article-categories><title-group><article-title>Dust resuspension from the splash of a falling powder: A numerical aerodynamic simulation of a pellet falling onto a powder monolayer</article-title></title-group><contrib-group><contrib contrib-type="author"><contrib-id contrib-id-type="orcid" authenticated="false">http://orcid.org/0000-0002-2831-2140</contrib-id><name><surname>Turkevich</surname><given-names>Leonid A.</given-names></name><xref rid="A1" ref-type="aff">a</xref></contrib><contrib contrib-type="author"><name><surname>Chen</surname><given-names>Hongyu</given-names></name><xref rid="A2" ref-type="aff">b</xref></contrib><contrib contrib-type="author"><name><surname>Jog</surname><given-names>Milind A.</given-names></name><xref rid="A2" ref-type="aff">b</xref></contrib></contrib-group><aff id="A1"><label>a</label>Division of Field Studies &#x00026; Engineering (DFSE), National Institute for Occupational Safety &#x00026; Health (NIOSH), The Centers for Disease Control &#x00026; Prevention (CDC), Alice Hamilton Laboratory, Cincinnati, Ohio, USA</aff><aff id="A2"><label>b</label>Thermal Fluids &#x00026; Thermal Processing Lab, Mechanical &#x00026; Materials Engineering, University of Cincinnati, Cincinnati, Ohio, USA</aff><author-notes><corresp id="CR1"><bold>CONTACT</bold> Leonid A. Turkevich, <email>LLT0@cdc.gov</email>, Division of Field Studies &#x00026; Engineering (DFSE), National Institute for Occupational Safety &#x00026; Health (NIOSH), The Centers for Disease Control &#x00026; Prevention (CDC), Alice Hamilton Laboratory, 1090 Tusculum Avenue, Cincinnati, OH 45226, USA.</corresp></author-notes><pub-date pub-type="nihms-submitted"><day>12</day><month>3</month><year>2025</year></pub-date><pub-date pub-type="ppub"><year>2025</year></pub-date><pub-date pub-type="pmc-release"><day>28</day><month>3</month><year>2025</year></pub-date><volume>59</volume><issue>1</issue><fpage>49</fpage><lpage>65</lpage><permissions><license><license-p>Full Terms &#x00026; Conditions of access and use can be found at <ext-link ext-link-type="uri" xlink:href="https://www.tandfonline.com/action/journalInformation?journalCode=uast20">https://www.tandfonline.com/action/journalInformation?journalCode=uast20</ext-link></license-p></license></permissions><abstract id="ABS1"><p id="P1">A falling powder can generate a dust cloud from its interaction with the ambient air and from its splash onto a substrate. This article reports the results of a numerical simulation study, which attempts to model this second process. We argue that the dust cloud arises from the aerodynamic resuspension of previously deposited small particles. The agglomerated falling powder is modeled as a falling pellet disk impacting a surface covered with a monolayer of previously deposited particles. The Reynolds number of the air flow in the vicinity of the impacting pellet is Re ~ 1860, so the air flow is modeled as laminar and incompressible. The dust particles are incorporated <italic toggle="yes">via</italic> a Lagrangian multiphase treatment. The sudden deceleration of the disk sheds an aerodynamic vortex, which suspends particles from the monolayer. Characteristics of the dust cloud (average and maximum height and radius) are tracked; these are conveniently summarized by following the trajectory of the dust cloud centroid. The probability of aerosolization decreases with distance from the impacted pellet. The centroid trajectory is studied as a function of dust particle size. The model is relatively insensitive to disk radius and thickness. More realistic modeling of dust clouds generated by the splash of falling powders will require a statistical analysis of aggregate size and location, as well as the inclusion of interparticle and particle-surface interactions.</p></abstract><abstract id="ABS2" abstract-type="graphical"><title>Graphical Abstract</title><p id="P2">
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</p></abstract></article-meta></front><body><sec id="S1"><label>1.</label><title>Introduction</title><sec id="S2"><label>1.1.</label><title>Motivation and outline</title><p id="P3">We are interested in sources of inhaled particulate exposure; a ubiquitous source is the dust generated by falling powders. There are two mechanisms for dust generation: aerosol that results intrinsically from the falling powder stream; aerosol that results from the &#x0201c;splash&#x0201d; of the powder as it impacts a surface. Modeling the first process is the subject of a forthcoming article. The current article presents the results of a simple model for this second &#x0201c;splash&#x0201d; process. We argue that dust generated by this &#x0201c;splash&#x0201d; process derives from the aerodynamic resuspension of particles previously deposited on the surface; the aerodynamic forces are associated with the decelerating powder agglomerates.</p><p id="P4">Resuspension has been actively studied for some time&#x02014;for a review, see <xref rid="R43" ref-type="bibr">Ferro (2022)</xref>. Most resuspension studies focus on overcoming the adhesive forces binding the particles to the substrate (<xref rid="R57" ref-type="bibr">John 1995</xref>). However, <xref rid="R26" ref-type="bibr">Cleaver and Yates (1973)</xref> investigated the role of turbulent flow at the surface in particle detachment. Our interest is in the bulk aerodynamics leading to detachment and in the subsequent evolution of the aerosol dust cloud.</p><p id="P5">We first review (<xref rid="S3" ref-type="sec">Section 1.2</xref>) real world sources of dust exposure and its measurement; we then focus (<xref rid="S4" ref-type="sec">Section 1.3</xref>) on falling powders and distinguish (<xref rid="S5" ref-type="sec">Section 1.4</xref>) the splash process; Section 1.5 defines our model of a descending pellet (representing an agglomerate) impacting a surface covered with a monolayer of primary particles. <xref rid="S6" ref-type="sec">Section 2</xref> summarizes our numerical methods. <xref rid="S13" ref-type="sec">Section 3</xref> discusses our results. <xref rid="S17" ref-type="sec">Section 4</xref> places our results in the context of the previous work by Shields on the (hydrodynamic) resuspension (of sediment) due to turbulent parallel flow.</p></sec><sec id="S3"><label>1.2.</label><title>Dust</title><p id="P6">Industrial powder handling represents a primary source of dust. Processes like powder spilling (<xref rid="R103" ref-type="bibr">Sutter, Johnston, and Mishima 1982</xref>), pouring (<xref rid="R52" ref-type="bibr">Heitbrink, Baron, and Willeke 1992</xref>), and conveying (<xref rid="R8" ref-type="bibr">Baker et al. 1986</xref>; <xref rid="R24" ref-type="bibr">Cheng 1973</xref>) can all lead to the generation of dust in occupational environments. Grinding and milling operations can also contribute to dust generation (<xref rid="R75" ref-type="bibr">Pensis et al. 2010</xref>). Conveyor transferring and the loading and unloading of bulk materials, like ore and agricultural products, can lead to dust generation (<xref rid="R23" ref-type="bibr">Chen et al. 2012</xref>; <xref rid="R94" ref-type="bibr">Shaw et al. 1998</xref>).</p><p id="P7">Dust can adversely affect human health. Silicosis, asbestosis, lung cancer, and heart disease are all related to dust exposure (<xref rid="R35" ref-type="bibr">Donaldson and Seaton 2012</xref>). Size and surface chemistry contribute to the toxicity of inhaled powders (<xref rid="R37" ref-type="bibr">Duffin et al. 2002</xref>, <xref rid="R38" ref-type="bibr">2007</xref>). The health hazards associated with exposure to nanoparticles are of current interest (<xref rid="R107" ref-type="bibr">Trout and Schulte 2010</xref>). Increased production and use of nanomaterials presage increased occupational exposure to dust from these materials (<xref rid="R41" ref-type="bibr">Evans et al. 2010</xref>; <xref rid="R58" ref-type="bibr">Kuhlbusch et al. 2011</xref>; <xref rid="R76" ref-type="bibr">Peters et al. 2008</xref>).</p><p id="P8">A free-falling powder is a common source of airborne dust, often occurring during a materials transfer process, or an accidental spill. Manual powder handling operations, such as silo or bag filling from a hopper, bag emptying, powder weigh-out, and powder transfer from a conveyor, all involve free-falling powders. The mechanisms of dust generation from free falling powders are not well understood.</p><p id="P9">Dustiness quantifies the ability of a finely divided solid (a powder) to become airborne as a dust aerosol when the powder is subjected to a mechanical or aerodynamical stimulus (<xref rid="R59" ref-type="bibr">Liden 2006</xref>; <xref rid="R78" ref-type="bibr">Plinke et al. 1995</xref>). Various dustiness measurement methods have been developed (<xref rid="R11" ref-type="bibr">BOHS 1985</xref>; <xref rid="R47" ref-type="bibr">Hamelmann and Schmidt 2003</xref>, <xref rid="R48" ref-type="bibr">2004</xref>, <xref rid="R49" ref-type="bibr">2005</xref>). Three types of dustiness testing methods are commonly used: the rotating drum method, the free-falling powder method, and the Venturi method. For a comprehensive review of dustiness test methods, see <xref rid="R40" ref-type="bibr">Evans (2024)</xref>. Field evaluations of worker dust exposure do not always correlate with dustiness test results (<xref rid="R13" ref-type="bibr">Brouwer et al. 2006</xref>; <xref rid="R53" ref-type="bibr">Heitbrink, Todd, and Fischbach 1989</xref>; <xref rid="R54" ref-type="bibr">Heitbrink et al. 1990</xref>; <xref rid="R85" ref-type="bibr">Ribalta et al. 2019</xref>).</p><p id="P10">Several historical dustiness test configurations utilize the falling powder geometry. Falling powder test systems can be of the single drop type, where a powder sample is dropped as a single bolus and impacts onto a solid surface, or the continuous falling type, where a continuous stream of powder winnows down a test chamber. Continuous falling methods tend to be more consistent than single drop methods (<xref rid="R12" ref-type="bibr">BOHS 1988</xref>); nonetheless, the majority of falling powder configurations are single-drop type.</p></sec><sec id="S4"><label>1.3.</label><title>Falling powder dustiness tests</title><p id="P11"><xref rid="R82" ref-type="bibr">Powell and Russell (1933)</xref> described a <italic toggle="yes">single-drop</italic> test with passive dust sampling to quantify coal and coke dust release; <xref rid="R6" ref-type="bibr">ASTM D547-41 (1980)</xref> standardized this test method. <xref rid="R11" ref-type="bibr">BOHS (1985)</xref> described a scaled down version with active particle samplers. <xref rid="R60" ref-type="bibr">Lundgren (1986)</xref> and <xref rid="R61" ref-type="bibr">Lundgren and Rangaraj (1986)</xref> similarly used active sampling. In a classical study, <xref rid="R1" ref-type="bibr">Andreasen, Hofman-Bang, and Rasmussen (1939)</xref> used the single drop technique to compare the dustiness of a wide range of materials against a lycopodium reference standard.</p><p id="P12">The Roaches Dust Particle Apparatus was developed to test dyestuffs (<xref rid="R10" ref-type="bibr">Berger-Schuun et al. 1989</xref>) and was later evaluated by <xref rid="R62" ref-type="bibr">Lyons and Mark (1992)</xref>. A single bolus of test powder falls into a quiescent chamber and impacts onto a base surface. In the Palas Dustview II version, the aerosol is optically monitored. <xref rid="R68" ref-type="bibr">O&#x02019;Shaughnessy, Kang, and Ellickson (2012)</xref> described a low mass variant of this test.</p><p id="P13"><xref rid="R14" ref-type="bibr">Burdett et al. (2000)</xref> describe a single drop test configuration with optical extinction detection, standardized as <xref rid="R34" ref-type="bibr">DIN 55992-2 (1999)</xref>. The test powder falls down a column; a gentle cross flow of air transports the dusty aerosol to size selective particle collection foams (<xref rid="R16" ref-type="bibr">CEN 1993</xref>; <xref rid="R56" ref-type="bibr">ISO 1995</xref>; <xref rid="R109" ref-type="bibr">Vincent et al. 1999</xref>). Splashing of the falling test powder from the impaction plate introduces variability. The Carr dispersibility test (<xref rid="R7" ref-type="bibr">ASTM 2021</xref>) measures the aerosolized dust as that gravimetric fraction of the dropped bolus that does not deposit on a collection surface at the base of the chamber.</p><p id="P14"><xref rid="R111" ref-type="bibr">Wells and Alexander (1978)</xref> described a <italic toggle="yes">continuous pour</italic> configuration. Dust is measured from air drawn horizontally across the falling powder. In the MRI (Midwest Research Institute) pouring device (<xref rid="R27" ref-type="bibr">Cowherd, Grelinger, and Wong 1989</xref>), a powder falls onto a powder covered receiving surface; a rotating, vibrating stainless-steel sample cup ensures a continuous stream of powder. EN15051-3 (<xref rid="R17" ref-type="bibr">CEN 2013</xref>) and EN17199-3 (<xref rid="R18" ref-type="bibr">CEN 2019</xref>) standardize a continuously metered falling powder test, performed against a slow countercurrent of upward moving air (<xref rid="R33" ref-type="bibr">Dahmann, Hartfiel, and Mocklinghoff 1997</xref>).</p><p id="P15">Computational Fluid Dynamics (CFD) has previously been used to study various dustiness testers. <xref rid="R36" ref-type="bibr">Dubey, Ghia, and Turkevich (2017)</xref> used CFD to investigate injection and sampling in the Venturi dustiness tester (VDT). The aerosolization within the VDT injection tube has also been investigated with CFD (<xref rid="R70" ref-type="bibr">Palakurthi 2017</xref>; <xref rid="R71" ref-type="bibr">Palakurthi, Ghia, and Turkevich 2017</xref>, <xref rid="R72" ref-type="bibr">2022</xref>; <xref rid="R91" ref-type="bibr">Sharma 2021</xref>; <xref rid="R92" ref-type="bibr">Sharma, Ghia, and Turkevich 2020a</xref>, <xref rid="R93" ref-type="bibr">2020b</xref>). <xref rid="R22" ref-type="bibr">Chen et al. (2021)</xref> and <xref rid="R21" ref-type="bibr">Chen, Jog, and Turkevich (2023)</xref> used CFD to investigate dust behavior in the standard (EN15051-2) and high-speed (Heubach) rotating drums. <xref rid="R89" ref-type="bibr">Schulz et al. (2019)</xref> used CFD-DEM to investigate the dustiness of bulk material handling in high-speed rotation drums as well as in the Palas Dust View apparatus. <xref rid="R20" ref-type="bibr">Chen et al. (2023)</xref> used CFD to study surface dust aerosolization by a turbulent parallel jet. <xref rid="R4" ref-type="bibr">Ansart et al. (2009</xref>, <xref rid="R5" ref-type="bibr">2011</xref>) and <xref rid="R3" ref-type="bibr">Ansart, de Ryck, and Dodds (2009)</xref> used an Euler-Euler multiphase model to investigate the intrinsic dust generation from a continuous falling powder.</p></sec><sec id="S5"><label>1.4.</label><title>The splash process</title><p id="P16"><xref rid="R51" ref-type="bibr">Heitbrink (1990)</xref> and coworkers (<xref rid="R52" ref-type="bibr">Heitbrink, Baron, and Willeke 1992</xref>) emphasized the additional dust generated by the &#x0201c;splash&#x0201d; of the powder from the substrate. A single bolus of powder fell either onto a flat plate or into a water-filled beaker. The difference in aerosol concentration caused by changing the impact surface was assumed to be the aerosol caused by processes that occur when the powder hits the flat plate. Two fine aluminum oxide powders were studied. Comparable contributions to the aerosol were generated from the powder as it falls and from the impact. The impact aerosol was enhanced in ultra-fines compared with the aerosol aerodynamically generated from the falling powder (<xref rid="R51" ref-type="bibr">Heitbrink 1990</xref>).</p><p id="P17">The <xref rid="R55" ref-type="bibr">Ibaseta-Biscans experiment (2007)</xref> was inspired by the MRI test (<xref rid="R28" ref-type="bibr">Cowherd et al. 1989</xref>). The powder was released from an invertible beaker; aerosol concentration and size distributions were measured at various heights. Two nanostructured powders were studied: anatase TiO<sub>2</sub> and fumed SiO<sub>2</sub>. Aerosol was produced by two mechanisms: dust generation from the falling powder and dust generation after impact on the chamber floor. Most of the aerosol was generated during the impact against the solid surface and then was upwardly convected. Once the aerosol was uniform in the chamber, the aerosol concentration decreased homogeneously <italic toggle="yes">via</italic> settling. We have visualized the second &#x0201c;splash&#x0201d; process in our laboratory.</p><p id="P18">A nominally 3&#x003bc;m calcium carbonate powder (Dust Chaser Fluorescent Leak Detector Powder from W. H. Kingsmill, Ltd., Burlington, ON, Canada: 75% calcium carbonate, 25% resin: 1,3-isobenzofurandiole polymer with 2,2-bis(hydroxymethyl)-1,3 propanediol to incorporate pink fluorescent pigment) is poured from a glass beaker, at a height of ~0.5m, onto a Plexiglas tray (with rim). The pouring powder is illuminated with UV light (100 LED Scorpion Master with peak <italic toggle="yes">&#x003bb;</italic>=390nm); the pouring process is recorded with a Camcorder (Hitachi DZ-BD10HA) at 30fps. The powder stream is intermittent (rather than continuous), reflecting cohesive agglomeration of the powder; the falling aggregates appear brightly illuminated (<xref rid="F1" ref-type="fig">Figure 1a</xref>).</p><p id="P19">After 0.3s, a fainter dust cloud (presumably consisting of smaller particles) rises from, and bounded by, the rim of, the Plexiglas tray (<xref rid="F1" ref-type="fig">Figure 1b</xref>). The particle size distribution (SEM analysis conducted by Maxxam, Bureau Veritas, Kennesaw, GA) of the original powder contains a significant submicron fraction (33.2% with <italic toggle="yes">l</italic>&#x0003c;1&#x003bc;m) in addition to the larger particles (41.2% with 1&#x003bc;m &#x0003c; <italic toggle="yes">l</italic> &#x0003c; 2&#x003bc;m; 15.6% with 2&#x003bc;m &#x0003c; <italic toggle="yes">l</italic> &#x0003c; 3&#x003bc;m; 6.3% with 3&#x003bc;m &#x0003c; <italic toggle="yes">l</italic> &#x0003c; 5&#x003bc;m; 2.9% with 5&#x003bc;m &#x0003c; <italic toggle="yes">l</italic> &#x0003c; 10&#x003bc;m; 0.8% with <italic toggle="yes">l</italic> &#x0003e; 10&#x003bc;m).</p></sec></sec><sec id="S6"><label>2.</label><title>Methods</title><sec id="S7"><label>2.1.</label><title>Modeling a falling powder</title><p id="P20">A falling powder generates dust <italic toggle="yes">via</italic> two processes: (a) dust generation directly by the falling powder (air-particle interaction&#x02014;upper part of figure), and (b) dust generation resulting from powder agglomerates impacting the bottom surface (lower part of figure) (<xref rid="F2" ref-type="fig">Figure 2</xref>).</p><p id="P21">In the first process, the falling powder entrains flow in the surrounding air (<xref rid="R17" ref-type="bibr">CEN 2013</xref>). The velocity gradient, between the falling powder and the quiescent air, transfers kinetic energy from the powder into air motion. The resultant air flow is complicated and is the subject of a future study.</p><p id="P22">In the second process, when agglomerated powder impacts the bottom surface, the accompanying air flow resuspends individual particles that had previously been deposited on the surface (<xref rid="R1" ref-type="bibr">Andreasen, Hofman-Bang, and Rasmussen 1939</xref>; <xref rid="R11" ref-type="bibr">BOHS 1985</xref>; <xref rid="R15" ref-type="bibr">Cawley and Leith 1993</xref>; <xref rid="R27" ref-type="bibr">Cowherd, Grelinger, and Wong 1989</xref>; <xref rid="R50" ref-type="bibr">Hammond 1980</xref>; <xref rid="R52" ref-type="bibr">Heitbrink, Baron, and Willeke 1992</xref>; <xref rid="R77" ref-type="bibr">Plinke, Leith, Boundy, et al. 1994</xref>; <xref rid="R81" ref-type="bibr">Plinke, Maus, and Leith 1992</xref>; <xref rid="R80" ref-type="bibr">Plinke et al. 1991</xref>). The present article reports the results of simulations of this second process. <xref rid="R79" ref-type="bibr">Plinke, Leith, Goodman, et al. (1994)</xref> studied the impaction force of falling powder agglomerates on the substrate.</p><p id="P23">Individual primary particles falling onto the bottom of the chamber do not contribute to the splash aerosol; they merely sediment at their Stokes terminal velocity. Large particle agglomerates falling to the bottom, or the collective motion of the dense particle stream impacting the bottom surface, generate strong vorticity in the vicinity of the bottom surface, which suspends previously deposited particles.</p><p id="P24">Our simulations study the aerodynamic dust generation resulting from the impact of the falling powder with the bottom surface. Falling agglomerates, or the collective motion of the falling powder, are modeled as a falling pellet disk. The pellet remains intact in this simulation. The powder hill at the base of the powder stream is modeled as a layer of particles. In our simulations, this layer of particles is released slightly above the bottom surface within 0.1s after the powder pellet impact. A result of our simulations is that the backflow generated by the falling disk (vortex shedding) is much more efficient than that from an impinging piston whose backflow at the surface merely derives from the displaced air ahead of the piston. A schematic of these simplifications is shown in the <xref rid="SD1" ref-type="supplementary-material">online supplemental information</xref> (<xref rid="SD1" ref-type="supplementary-material">SI, Section S-1</xref>).</p><p id="P25">The model geometry is inspired by the Heitbrink experiments (<xref rid="R52" ref-type="bibr">Heitbrink, Baron, and Willeke 1992</xref>). The test chamber is a column of 75cm in height with a square 12 &#x000d7; 12cm base. The standard pellet in the simulations is a cylindrical disk of 4mm radius and 3mm thickness. The size of the pellet is clearly much larger than a typical agglomerate; however, we argue (see the <xref rid="SD1" ref-type="supplementary-material">SI&#x02014;Section S-6</xref>) that the physics of the splash process is relatively insensitive to the size of the pellet. For specificity, the powder and pellet are modeled as silica, with density <italic toggle="yes">&#x003c1;</italic> = 2000kg/m<sup>3</sup>; the pellet has a mass of 3.0144 &#x000d7; 10<sup>&#x02212;4</sup> kg. It is released from the top of the test chamber; for numerical stability of the simulation, the release is gradually ramped up, with the full gravitational acceleration only achieved after &#x00394;<italic toggle="yes">t</italic>=0.25s. Physically, the orientation of a falling disk would be unstable, with the disk tumbling (<xref rid="R45" ref-type="bibr">Field et al. 1997</xref>; <xref rid="R118" ref-type="bibr">Zhong, Chen, and Lee 2011</xref>; <xref rid="R119" ref-type="bibr">Zhong et al. 2013</xref>); in our simulations, the disk is constrained to fall with its flat always oriented horizontally, i.e., parallel to the bottom surface. Again, for numerical stability of the simulation, the pellet disk is not allowed to impact the bottom of the test chamber, but rather, the fall of the disk is halted 1mm above the bottom of the test chamber. Halting the pellet descent just before impact also isolates the aerodynamic resuspension mechanism (studied here) from other forces between the pellet and the particles that are to be resuspended.</p><p id="P26">The final velocity of the pellet is 3.64m/s, achieved at &#x00394;<italic toggle="yes">t</italic>~0.515s from release. The final velocity is reduced by 10% due to the ramping up of gravity; similarly, the impact time is delayed by 32% due to the ramping up of gravity. Only the final impact velocity is relevant for the dust cloud generation. This final velocity is only &#x000bc; of the estimated terminal velocity (balancing gravitational acceleration against Stokes drag). For a discussion of the terminal velocity of disk-shaped particles, see <xref rid="R121" ref-type="bibr">Zhou et al. (2022)</xref>. Since all velocities are low, the air is treated as incompressible. The Reynolds number for this final air flow around the pellet is Re ~ 1860. For 40 &#x0003c; Re &#x0003c; 105, the flow pattern is expected to be symmetric about the central axis of the disk, with a recirculation zone behind the disk. For Re ~ 105, the wake behind the disk is expected to lose axial symmetry, with long thin thread-like wakes extending behind a pair of recirculation zones (<xref rid="R67" ref-type="bibr">Natarajan and Acrivos 1993</xref>; <xref rid="R120" ref-type="bibr">Zhong and Lee 2012</xref>). Periodic vortex shedding is expected to occur for Re &#x0003e; 118 (<xref rid="R9" ref-type="bibr">Bearman and Takamoto 1988</xref>; <xref rid="R42" ref-type="bibr">Fabre, Auguste, and Magnaudet 2008</xref>; <xref rid="R63" ref-type="bibr">Miau et al. 1997</xref>; <xref rid="R95" ref-type="bibr">Shenoy and Kleinstreuer 2008</xref>; <xref rid="R120" ref-type="bibr">Zhong and Lee 2012</xref>). Vortex generation behind accelerating and decelerating disks has also been studied (<xref rid="R87" ref-type="bibr">Sallet 1975</xref>; <xref rid="R99" ref-type="bibr">Steiner et al. 2023</xref>; <xref rid="R106" ref-type="bibr">Taylor 1953</xref>; <xref rid="R116" ref-type="bibr">Yang, Jia, and Yin 2012</xref>).</p><p id="P27">Spherical particles are uniformly distributed as a monolayer at the bottom of the chamber and are released at &#x00394;<italic toggle="yes">t</italic>=0.6s after the release of the disk at the top, i.e., within 0.1s after the disk is stopped at the bottom. Releasing the particles just above the substrate deliberately neglects particle-substrate interactions (the focus of traditional resuspension studies, which emphasize overcoming the adhesion forces to the substrate). There are no particle-particle interactions and no particle agglomeration or break-up. Particle collisions with the chamber wall are treated as elastic. The simulations are athermal. The simulations are thus designed to isolate and highlight the role of aerodynamics in the resuspension process.</p></sec><sec id="S8"><label>2.2.</label><title>Numerical methods</title><p id="P28">We have used <xref rid="R97" ref-type="bibr">STAR-CCM+ (2023)</xref> as the CFD simulation software in this study. STAR-CCM+ can easily track massive particle trajectories. For a general discussion of modeling dilute particle-laden flows, see <xref rid="R19" ref-type="bibr">Chen and Wood (1985)</xref>, <xref rid="R29" ref-type="bibr">Crowe (1998)</xref>, <xref rid="R32" ref-type="bibr">Curtis and van Wachem (2004)</xref>, <xref rid="R90" ref-type="bibr">Schwarzkopf, Crowe, and Dutta (2009)</xref>, <xref rid="R108" ref-type="bibr">Tsuji, Morikawa, and Shiomi (1984)</xref>, and <xref rid="R117" ref-type="bibr">Zhang and Reese (2001)</xref>.</p></sec><sec id="S9"><label>2.3.</label><title>Grid generation</title><p id="P29">The domain is the Heitbrink chamber (75 &#x000d7; 12 &#x000d7; 12cm). Unstructured grids (<xref rid="R44" ref-type="bibr">Ferziger, Peric, and Street 2019</xref>) were generated within STAR-CCM+; the basic cell is a 3mm cube (&#x02018;trimmed cell&#x02019;) in the bulk of the domain and flattened rectangular prisms at the disk boundary surface. Near the bottom surface (5 &#x000d7; 12 &#x000d7; 12cm), the grid is 50% refined (refined cell is a 1.5cm cube). The central column (75 &#x000d7; 5 &#x000d7; 5cm) is also 50% refined. The total cell count is 1,131,386. The falling disk is treated as a moving part. The refined grid in the central cylinder rigidly moves with the falling disk. A schematic of the grid geometry is given in the <xref rid="SD1" ref-type="supplementary-material">SI</xref> (<xref rid="SD1" ref-type="supplementary-material">Section SM-2</xref>).</p></sec><sec id="S10"><label>2.4.</label><title>Numerical simulation method</title><sec id="S11"><label>2.4.1.</label><title>Air flow only</title><p id="P30">The final velocity of the pellet is <italic toggle="yes">v<sub>f</sub></italic>=3.64m/s. This sets the velocity scale of the air flow in the chamber, whence <italic toggle="yes">v</italic>/<italic toggle="yes">c</italic><sub>sound</sub> &#x0003c; 10<sup>&#x02212;2</sup>, where <italic toggle="yes">c</italic><sub>sound</sub> is the velocity of sound in air; the flow is thus incompressible. The final pellet velocity is achieved at &#x00394;<italic toggle="yes">t</italic>~0.54s from release; note that this is only &#x000bc; of the terminal velocity (balancing gravitational acceleration against Stokes drag). The Reynolds number for this final air flow around the pellet is Re ~ 1860. The air flow near the bottom surface is smaller and quickly dissipates after pellet impact; the air flow is thus treated as laminar.</p><p id="P31">The finite volume method (FVM) is used to discretize the governing equations. The discretization of equations and domain, as well as the iterations of discretized equations, are all conducted using the commercial FVM solver within STAR-CCM+. The convection terms are discretized using a second-order Upwind Scheme. The transient terms are discretized by a second-order Temporal Scheme. The time step is set at &#x00394;<italic toggle="yes">t</italic>=0.0025s, and the simulation is run for &#x00394;<italic toggle="yes">T</italic>=40s. The discretized governing equations are solved using the SIMPLE (Semi-Implicit Method for Pressure Linked Equations) algorithm. Velocity and pressure under-relaxation factors are 0.9 and 0.5, respectively. The falling disk is incorporated using rigid motion of the core cylindrical grid. The solution of the equations was considered to be converged when the scaled residuals for the continuity and momentum equations decreased to 10<sup>&#x02212;5</sup> for each time step. Grid independence of the air flow solutions is discussed in the <xref rid="SD1" ref-type="supplementary-material">SI&#x02014;Section S-3</xref>.</p></sec><sec id="S12"><label>2.4.2.</label><title>Addition of particles&#x02014;Lagrangian multiphase approach</title><p id="P32">To simulate the dust cloud lofting, the particles are initially distributed uniformly on the bottom of the entire chamber. The number of particles in the simulations was <italic toggle="yes">N</italic>=10<sup>4</sup> for the dustiness simulations and <italic toggle="yes">N</italic>=10<sup>2</sup> for the particle track simulations. Particles are injected at <italic toggle="yes">t</italic>=0.6s (using the Star CCM+ Parcel Injector) with an initial upward velocity of <italic toggle="yes">v</italic>=1 &#x000d7; 10<sup>&#x02212;6</sup>m/s.</p><p id="P33">Lagrangian Multiphase flow (<xref rid="R101" ref-type="bibr">Subramaniam 2013</xref>; <xref rid="R105" ref-type="bibr">Tartakovsky, Ferris, and Meakin 2009</xref>) incorporates air-particle interaction by adding air source terms into the Navier-Stokes equations (<xref rid="R2" ref-type="bibr">Andrews and O&#x02019;Rourke 1996</xref>; <xref rid="R29" ref-type="bibr">Crowe 1998</xref>; <xref rid="R31" ref-type="bibr">Crowe, Troutt, and Chung 1996</xref>; <xref rid="R30" ref-type="bibr">Crowe et al. 2011</xref>; <xref rid="R73" ref-type="bibr">Patankar and Joseph 2001a</xref>, <xref rid="R74" ref-type="bibr">2001b</xref>; <xref rid="R90" ref-type="bibr">Schwarzkopf, Crowe, and Dutta 2009</xref>; <xref rid="R98" ref-type="bibr">Snider, O&#x02019;Rourke, and Andrews 1998</xref>). For a dilute dust cloud (volume fraction <italic toggle="yes">&#x003d5;</italic> &#x0003c; 10<sup>&#x02212;3</sup>), the main air-particle forces (<xref rid="R30" ref-type="bibr">Crowe et al. 2011</xref>) are drag (<xref rid="R88" ref-type="bibr">Schiller and Naumann 1935</xref>; <xref rid="R100" ref-type="bibr">Stokes 1851</xref>) and particle shear-lift (<xref rid="R86" ref-type="bibr">Saffman 1965</xref>); gravitational body force is incorporated in the usual way.</p><p id="P34">Tracking of massive particles is incorporated <italic toggle="yes">via</italic> the Lagrangian-Euler Method with two-way coupling between the air continuum and the dispersed particulate phase. Particle&#x02013;particle interactions are neglected. Particle agglomeration and breakup are also neglected since aerodynamic shear forces are insufficient to break up agglomerates. For the Heitbrink geometry, we do not expect particle impact on the chamber walls, which, in principle, might induce breakup, so this also has been neglected. The infrequent interaction of the particles with the chamber walls has been specified to be purely elastic (i.e., unit coefficient of restitution), so no particles stick to the chamber walls.</p><p id="P35">In the Lagrangian-Euler Method, the motion of each dust particle in the Lagrangian frame is given by:
<disp-formula id="FD1">
<label>(1)</label><mml:math id="M1" display="block"><mml:mrow><mml:msub><mml:mi>m</mml:mi><mml:mi>p</mml:mi></mml:msub><mml:mfrac><mml:mrow><mml:msub><mml:mi mathvariant="italic">dv</mml:mi><mml:mi>p</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="italic">dt</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:msub><mml:mi>F</mml:mi><mml:mi>d</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>F</mml:mi><mml:mi>p</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mi mathvariant="italic">LS</mml:mi></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>m</mml:mi><mml:mi>p</mml:mi></mml:msub><mml:mi>g</mml:mi></mml:mrow></mml:math>
</disp-formula>
where <italic toggle="yes">m<sub>p</sub></italic> and <italic toggle="yes">v<sub>p</sub></italic> are the mass and velocity of the particle and <italic toggle="yes">g</italic> is the gravitational acceleration. The drag force, <italic toggle="yes">F<sub>d</sub></italic>, and pressure force, <italic toggle="yes">F<sub>p</sub></italic>, are given below. The drag force (in a direction opposite to the motion of the particle) is given by
<disp-formula id="FD2">
<label>(2)</label><mml:math id="M2" display="block"><mml:mrow><mml:msub><mml:mi>F</mml:mi><mml:mi>d</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac><mml:msub><mml:mi>C</mml:mi><mml:mi>d</mml:mi></mml:msub><mml:mi>&#x003c1;</mml:mi><mml:msub><mml:mi>A</mml:mi><mml:mi>p</mml:mi></mml:msub><mml:msubsup><mml:mi>v</mml:mi><mml:mi>r</mml:mi><mml:mn>2</mml:mn></mml:msubsup></mml:mrow></mml:math>
</disp-formula>
where <italic toggle="yes">A<sub>p</sub></italic>=(<italic toggle="yes">&#x003c0;</italic>/2) <italic toggle="yes">D<sub>p</sub><sup>2</sup></italic> is the particle cross-sectional area, <italic toggle="yes">D<sub>p</sub></italic> is the particle diameter, <italic toggle="yes">&#x003c1;</italic> is the density of air, and the relative particle-air velocity <italic toggle="yes">v<sub>r</sub></italic>=<italic toggle="yes">u</italic> &#x02212; <italic toggle="yes">v<sub>p</sub></italic>, where <italic toggle="yes">u</italic> is the local air velocity, <italic toggle="yes">v<sub>p</sub></italic> is the local particle velocity, and where <italic toggle="yes">C<sub>d</sub></italic> is the <xref rid="R88" ref-type="bibr">Schiller-Naumann particle drag coefficient (1935)</xref>. The pressure gradient force is given by
<disp-formula id="FD3">
<label>(3)</label><mml:math id="M3" display="block"><mml:mrow><mml:msub><mml:mi>F</mml:mi><mml:mi>p</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mo>&#x02212;</mml:mo><mml:msub><mml:mi>V</mml:mi><mml:mi>p</mml:mi></mml:msub><mml:mo>&#x02207;</mml:mo><mml:msub><mml:mi>p</mml:mi><mml:mrow><mml:mi mathvariant="italic">static</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math>
</disp-formula>
where <italic toggle="yes">V<sub>p</sub></italic>=(<italic toggle="yes">&#x003c0;</italic>/6) <italic toggle="yes">D<sub>p</sub><sup>3</sup></italic> is the particle volume, and &#x02207;<italic toggle="yes">p<sub>static</sub></italic> is the gradient of the static air pressure. There is an additional Safman lift force, <italic toggle="yes">F<sub>LS</sub></italic>, on each particle, due to shear near the walls (<xref rid="R86" ref-type="bibr">Saffman 1965</xref>).</p><p id="P36">We have used two-way coupling for these simulations. A result of our simulations is that the particles remained well-dispersed in the cloud; the aerosol is thus sufficiently dilute so that one-way coupling would have been sufficient. However, we wanted to admit the possibility of particles accumulating in a localized region of the cloud, in which case, the feedback of the particle motion on the fluid would become important, necessitating two-way coupling.</p><p id="P37">In two-way coupling, the rate of momentum transfer from the particles back to the continuum air phase is achieved by augmenting the Navier-Stokes equations with a sink term
<disp-formula id="FD4">
<label>(4)</label><mml:math id="M4" display="block"><mml:mrow><mml:msub><mml:mtext>S</mml:mtext><mml:mtext>V</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mo>&#x02212;</mml:mo><mml:msub><mml:mstyle stretchy="true"><mml:mo>&#x02211;</mml:mo></mml:mstyle><mml:mi>n</mml:mi></mml:msub><mml:mrow><mml:msubsup><mml:mi>F</mml:mi><mml:mi>d</mml:mi><mml:mi>n</mml:mi></mml:msubsup><mml:mrow><mml:mrow><mml:mi>&#x003b4;</mml:mi><mml:msub><mml:mi>t</mml:mi><mml:mi>n</mml:mi></mml:msub></mml:mrow><mml:mo>/</mml:mo><mml:mrow><mml:mtext>&#x00394;</mml:mtext><mml:mi>t</mml:mi></mml:mrow></mml:mrow></mml:mrow></mml:mrow></mml:math>
</disp-formula>
where the sum is over all particles <italic toggle="yes">n</italic> in the given cell during the computed time step, <italic toggle="yes">F<sub>d</sub><sup>n</sup></italic> is the drag force (<xref rid="FD2" ref-type="disp-formula">2</xref>) exerted by the fluid on the <italic toggle="yes">n</italic>th particle, and <italic toggle="yes">&#x003b4;</italic><italic toggle="yes">t<sub>n</sub></italic>/&#x00394;<italic toggle="yes">t</italic> is the fraction of time that the <italic toggle="yes">n</italic>th particle spends in the given cell during this time step.</p></sec></sec></sec><sec id="S13"><label>3.</label><title>Results and discussion</title><sec id="S14"><label>3.1.</label><title>Airflow of the standard falling pellet</title><p id="P38">We first discuss the air flow generated by the falling pellet disk (<italic toggle="yes">R</italic>=4mm, <italic toggle="yes">t</italic>=3mm). As the disk falls, it induces air motion within the chamber (<xref rid="SD1" ref-type="supplementary-material">SI Figure S-5</xref>). After &#x00394;<italic toggle="yes">t</italic>~0.3s, Re &#x0003e; 100, and vortices are shed behind the disk; the flow behind the disk is asymmetric and unstable. Air ahead of the disk is quiescent. The disk &#x0201c;impacts&#x0201d; the bottom of the chamber at <italic toggle="yes">t</italic>=0.54s. Particles will be released at 0.6s. As the pellet impacts, the edges of the disk are regions of high vorticity (<xref rid="SD1" ref-type="supplementary-material">SI Figure S-6</xref>). Radial and upward air flow has the potential to loft particles up from the surface and aerosolize a dust cloud.</p><p id="P39"><xref rid="F3" ref-type="fig">Figure 3</xref> shows the vertical velocity, <italic toggle="yes">v<sub>y</sub></italic>, on the central midplane (<italic toggle="yes">z</italic>=0) just before (<italic toggle="yes">t</italic>=0.5s&#x02014;panel a) and just after impact (<italic toggle="yes">t</italic>=0.6s&#x02014;panel b); height axis is left-to-right (the top of the chamber is at left; the base of the chamber is at right); cross-plane distance is front-to-back. We are particularly interested in the air flow induced at the base of the chamber, which will be instrumental in lofting dust from the monolayer. Before impact, the downward vertical velocity is confined to the wake immediately <italic toggle="yes">behind</italic> the disk (there is negligible flow ahead of the disk, arguing against the importance of piston-like flow driving dust dispersion); a small region of upward velocity exists just outside the disk, presumably from the attached vortex ring around the disk. Upon impact, the region of upward velocity extends from the disk radius outwards all the way toward the chamber walls. A full time sequence of the evolution of the vertical velocity is given in the <xref rid="SD1" ref-type="supplementary-material">SI</xref> (<xref rid="SD1" ref-type="supplementary-material">Figure S-7</xref>).</p><p id="P40"><xref rid="F4" ref-type="fig">Figure 4</xref> shows the out-of-plane vorticity magnitude, |<italic toggle="yes">&#x003c9;<sub>z</sub></italic>|, on the central midplane (<italic toggle="yes">z</italic>=0) just before (<italic toggle="yes">t</italic>=0.5s&#x02014;panel a) and just after impact (<italic toggle="yes">t</italic>=0.6s&#x02014;panel b); height axis is left-to-right (the top of the chamber is at left; the base of the chamber is at right); cross-plane distance is front-to-back. Again, we are interested in the air flow induced at the base of the chamber, which will be instrumental in lofting dust from the monolayer. Before impact, there is large positive/negative vorticity on the right/left of the disk, indicative of the vortex ring attached to the disk; again, vorticity is confined to the wake <italic toggle="yes">behind</italic> the pellet. Upon impact, the vorticity dissipates radially. We interpret this behavior as the detachment of the bound trailing vortex ring upon deceleration of the pellet. A full sequence of the out-of-plane vorticity, <italic toggle="yes">&#x003c9;<sub>z</sub></italic> is given in the <xref rid="SD1" ref-type="supplementary-material">SI</xref> (<xref rid="SD1" ref-type="supplementary-material">Figure S-8</xref>).</p></sec><sec id="S15"><label>3.2.</label><title>Standard pellet&#x02014;standard dust</title><p id="P41">In this section, we discuss the dust cloud generated by the impact of the standard pellet disk (<italic toggle="yes">R</italic>=4mm, <italic toggle="yes">t</italic>=3mm) on a monolayer of 1 &#x003bc;m silica particles. The dust cloud develops with time, as shown in <xref rid="F5" ref-type="fig">Figure 5</xref>. The pellet has impacted at <italic toggle="yes">t</italic>=0.54s (before the first panel). The wake behind the decelerated disk evinces the residual motion (velocities depicted with the color scale) due to previous vortex shedding; this persists for long time (it is still apparent at <italic toggle="yes">t</italic>=20s). At the bottom of the chamber, the lofted particle dust cloud is indicated in dark blue. Due to the small particle size (<italic toggle="yes">d</italic>=1&#x003bc;m), the dust cloud does not settle with time. Note the scale: the chamber height is 75cm; the apparent dust cloud height is of the order of several cm.</p><p id="P42">Pictures showing the temporal evolution of dustiness, average height, and radius of the dust cloud are given in the <xref rid="SD1" ref-type="supplementary-material">SI</xref> (<xref rid="SD1" ref-type="supplementary-material">Section S-5</xref>). For the purposes of the simulation, dustiness is operationally defined as the fraction of particles that are lofted above <italic toggle="yes">y</italic>=5mm. <xref rid="SD1" ref-type="supplementary-material">Figure S-9</xref> displays the dustiness as a function of time. Within 0.5s of impact, 14% of the monolayer has been aerosolized (note that the magnitude of this fraction is somewhat arbitrary, as it would be reduced for a chamber of larger base size). This time for aerosolization is comparable to what we observed (0.3s) in our visualization of the splash process (<xref rid="F1" ref-type="fig">Figure 1</xref>). Due to their small size, the particles remain suspended for the duration of the simulation (40s). The persistence of the splash dust cloud is consistent with our observation (<xref rid="F1" ref-type="fig">Figure 1</xref>).</p><p id="P43"><xref rid="SD1" ref-type="supplementary-material">Figure S-10</xref> displays the height of the dust cloud. The maximum height (height of the highest particle) is ~20 times the average height (averaging the height over all particles). This indicates that the dust cloud density decreases with height, as expected. It also indicates that the dust cloud is not vertically well-mixed over its entire height. The constancy of that ratio suggests that the structure of the dust cloud does not change with time. The lack of vertical mixing is consistent with our observation (<xref rid="F1" ref-type="fig">Figure 1</xref>).</p><p id="P44"><xref rid="SD1" ref-type="supplementary-material">Figure S-11</xref> displays the average radius of the dust cloud (averaging the radial location over all particles). Within 0.5s, the extent of the dust cloud quickly expands to 4.5cm, which is an order of magnitude larger than the disk radius, and seems to be limited by the confining walls of the chamber; we cannot measure the intrinsic radius (with no confining chamber walls) of the dust cloud in these simulations. The small undulation for 2s &#x0003c; <italic toggle="yes">t</italic> &#x0003c; 6s suggests that while the cloud is initially propelled outward, it undergoes a minor retraction during this time interval (possibly driven by the motion of the vortex ring detaching from the fallen disk). The simulation lateral extent (4.5cm) is larger than that of our visualization (<xref rid="F1" ref-type="fig">Figure 1</xref>), but our experimental dust cloud may be more confined due to the retaining wall of the Plexiglas tray into which the powder falls.</p><p id="P45">The average dust cloud height and radius may be combined to monitor the trajectory of the dust cloud centroid (note that this is not the center of mass, which would be located at <italic toggle="yes">r</italic>=0, above the pellet). <xref rid="F6" ref-type="fig">Figure 6</xref> displays the trajectory of the centroid for 0.6s &#x0003c; <italic toggle="yes">t</italic> &#x0003c; 10s. The dust cloud starts near the floor (<italic toggle="yes">r</italic>=2.6cm, <italic toggle="yes">h</italic>=9mm) at <italic toggle="yes">t</italic>=0.6s and is propelled outward and lofted (<italic toggle="yes">r</italic>=43cm, <italic toggle="yes">h</italic>=7.3cm) at <italic toggle="yes">t</italic>=10s. At intermediate times (<italic toggle="yes">t</italic>~2s), there is a slight retraction in radius with no additional lofting, and then lofting recommences with an additional expansion; at later times (<italic toggle="yes">t</italic>&#x0003e;8s) there is a slight retraction as lofting continues but is considerably slowed.</p><p id="P46">We have also conducted simulations where the initial monolayer of particles does not cover the entire floor of the chamber but rather is confined to a sequence of annuli around the pellet impact point. This allows a calculation of dustiness as a function of radial distance from the impacting disk (<xref rid="F7" ref-type="fig">Figure 7</xref>). Note that this dustiness &#x0201c;profile&#x0201d; does not give information on the structure of the dust cloud; rather, it represents the probability of resuspension as a function of distance from the impacting disk. As expected, aerosolization is complete (dustiness ~ 1) near the impacting disk; the probability decreases to ~0.5 at ~5 times the radius of the disk; the probability effectively vanishes at ~10 times the radius of the disk. This dustiness profile is time-independent, reflecting the lack of settling of the dust cloud of 1&#x003bc;m particles.</p><p id="P47">We also can follow the centroid trajectory of the cloud resuspended from each of these annular monolayers (<xref rid="SD1" ref-type="supplementary-material">Figure S-12</xref>). Each annulus, once resuspended, is propelled radially outward as lofting progresses. Each annulus experiences a retraction (2s &#x0003c; <italic toggle="yes">t</italic> &#x0003c; 4s) before it resumes expansion and lofting. For <italic toggle="yes">t</italic> &#x0003e; 4s, the trajectories of all but the outermost annulus coincide, suggesting radial mixing of the particles originating from these different annuli.</p><p id="P48">We have also monitored the number of particles aerosolized to different height slabs (0&#x02013;0.5, 0.5&#x02013;5, 5&#x02013;10, 10&#x02013;15, 15&#x02013;20, 20&#x02013;25cm). Inverting the measured average particle radius within each height slab permits a determination of the dust cloud profile (<xref rid="F8" ref-type="fig">Figure 8</xref>). For small times (<italic toggle="yes">t</italic>=1s), the dust profile monotonically decreases away from the fallen pellet. At <italic toggle="yes">t</italic>=2.5s, the extrema of the cloud are propelled outward; at <italic toggle="yes">t</italic>=5s, intermediate heights are retracted inward. For <italic toggle="yes">t</italic> &#x0003e; 10s, the dust profile returns to being monotonic, as the lofting proceeds. For 20s &#x0003c; <italic toggle="yes">t</italic> &#x0003c; 40s, lofting has stabilized with the cloud retracting inward somewhat.</p><p id="P49">The model is relatively insensitive to variations in pellet radius and thickness (<xref rid="SD1" ref-type="supplementary-material">SI&#x02014;Section S-6</xref>).</p></sec><sec id="S16"><label>3.3.</label><title>Dust particle size effects</title><p id="P50">We now study changes in the dust cloud as the size of the particle in the monolayer is changed. Dustiness (the fraction of particles that have been lofted above 5mm height in the chamber) depends upon particle diameter (<xref rid="F9" ref-type="fig">Figure 9</xref>). While the initial lofting of the dust cloud is independent of powder particle size, at longer times, gravitational settling reduces the particle population in the dust cloud. Gravitational settling is apparent at <italic toggle="yes">d</italic>=5&#x003bc;m; for <italic toggle="yes">d</italic>=7.5&#x003bc;m, the dust cloud settles over the timescale of the experiment (<italic toggle="yes">t</italic>=40s).</p><p id="P51">The depletion of particles from the dust cloud also affects the height of the dust cloud. We monitor this change by looking at the cloud centroid trajectories for powders of different particle diameters (<xref rid="F10" ref-type="fig">Figure 10</xref>). For particles with <italic toggle="yes">d</italic>&#x0003c;5&#x003bc;m, the trajectories are identical to those of the 1&#x003bc;m dust cloud; for particles with <italic toggle="yes">d</italic>&#x0003e;15&#x003bc;m, gravitational settling precludes significant lofting; dust clouds for the intermediate particle sizes exhibit erratic cross-over between the small and large particle clouds.</p><p id="P52">Taking vertical sections, we may track the change in the temporal dust cloud profile as a function of particle size (<xref rid="F11" ref-type="fig">Figure 11</xref>). Cloud height begins to decrease at <italic toggle="yes">d</italic>=5&#x003bc;m and is significant at <italic toggle="yes">d</italic>=10&#x003bc;m. The radial cloud retraction (<italic toggle="yes">t</italic>~5s) is apparent for clouds with <italic toggle="yes">d</italic>&#x0003c;7.5&#x003bc;m.</p></sec></sec><sec id="S17"><label>4.</label><title>Discussion&#x02013;relevant aerodynamics</title><p id="P53"><xref rid="R39" ref-type="bibr">Eames and Dalziel (2000)</xref> studied experimentally the hydrodynamic resuspension of dust particles from a surface due to the flow disturbance generated by an impacting body (300 &#x0003c; Re &#x0003c; 3500). They concluded that dust resuspension occurs if the <xref rid="R96" ref-type="bibr">Shields criterion (1936)</xref> (developed for horizontal transport of sediment by a turbulent parallel flow) is satisfied. The particle Shields parameter is defined as
<disp-formula id="FD5">
<label>(5)</label><mml:math id="M5" display="block"><mml:mrow><mml:msub><mml:mi>&#x003b8;</mml:mi><mml:mi>P</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mrow><mml:mo>[</mml:mo><mml:mrow><mml:mrow><mml:mrow><mml:msub><mml:mi>&#x003c1;</mml:mi><mml:mi>f</mml:mi></mml:msub></mml:mrow><mml:mo>/</mml:mo><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:msub><mml:mi>&#x003c1;</mml:mi><mml:mi>P</mml:mi></mml:msub><mml:mo>&#x02212;</mml:mo><mml:msub><mml:mi>&#x003c1;</mml:mi><mml:mi>f</mml:mi></mml:msub></mml:mrow><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:mrow></mml:mrow><mml:mo>]</mml:mo></mml:mrow><mml:mrow><mml:mrow><mml:msup><mml:mi>U</mml:mi><mml:mn>2</mml:mn></mml:msup></mml:mrow><mml:mo>/</mml:mo><mml:mrow><mml:mi mathvariant="italic">gd</mml:mi></mml:mrow></mml:mrow></mml:mrow></mml:math>
</disp-formula>
where <italic toggle="yes">U</italic> is the impacting velocity and <italic toggle="yes">d</italic> is the particle diameter; <italic toggle="yes">&#x003c1;</italic><italic toggle="yes"><sub>p</sub></italic> and <italic toggle="yes">&#x003c1;</italic><sub><italic toggle="yes">f</italic></sub> are, respectively, the particle and fluid densities. Resuspension occurs when <italic toggle="yes">&#x003b8;<sub>p</sub></italic> &#x0003e; <italic toggle="yes">&#x003b8;<sub>c</sub></italic> where the critical Shields parameter <italic toggle="yes">&#x003b8;<sub>c</sub></italic> ~ 5/Re<sub><italic toggle="yes">p</italic></sub><sup>1/2</sup> for Re<sub><italic toggle="yes">p</italic></sub> &#x0003c; 1 and <italic toggle="yes">&#x003b8;<sub>c</sub></italic> ~ 3 for Re<sub><italic toggle="yes">p</italic></sub> &#x0003e; 1, where Re<sub><italic toggle="yes">p</italic></sub> is the particle Reynolds number. <xref rid="F12" ref-type="fig">Figure 12</xref> displays the maximum diameter of a Shields suspendable dust particle at a given impact velocity, <italic toggle="yes">U</italic>; our simulations (vertical line at <italic toggle="yes">U</italic>=3.64m/s) are all consistent with the Shields criterion.</p><p id="P54"><xref rid="R102" ref-type="bibr">Sutherland (1967)</xref> imaged the motion of a grain on a surface, due to an impacting vortex ring (generated by a pulsating normal jet); he reported a threshold pulse frequency for the generation of particle motion and crater formation in the sediment. <xref rid="R112" ref-type="bibr">Wells (1992)</xref> and <xref rid="R113" ref-type="bibr">Wells and Hopfinger (1993)</xref> studied trajectories and kinematics of individual particles suspended by the impact of a low Re ~ 25 vortex ring; the Wells trajectories closely resemble the dust centroid trajectories of our study (<xref rid="F6" ref-type="fig">Figures 6</xref>, <xref rid="F10" ref-type="fig">10</xref>, <xref rid="SD1" ref-type="supplementary-material">S-12</xref>). <xref rid="R65" ref-type="bibr">Munro, Bethke, and Dalziel (2009)</xref> studied the crater formation in a sediment due to the normal impact of a vortex ring (Re ~ 5000).</p><p id="P55">The interaction of a vortex ring directly impacting a wall has been extensively studied (<xref rid="R25" ref-type="bibr">Chu, Wang, and Chang 1995</xref>; <xref rid="R46" ref-type="bibr">Gendrich, Bohl, and Koochesfahani 1997</xref>; <xref rid="R64" ref-type="bibr">Mishra, Pumir, and Ostilla-M&#x000f3;nico 2021</xref>; <xref rid="R66" ref-type="bibr">Naguib and Koochesfahani 2004</xref>; <xref rid="R69" ref-type="bibr">Orlandi and Verzicco 1993</xref>; <xref rid="R84" ref-type="bibr">Ren, Zhang, and Guan 2016</xref>; <xref rid="R83" ref-type="bibr">Ren and Lu 2015</xref>; <xref rid="R104" ref-type="bibr">Swearingen, Crouch, and Handler 1995</xref>; <xref rid="R110" ref-type="bibr">Walker et al. 1987</xref>; <xref rid="R115" ref-type="bibr">Xu et al. 2017</xref>; <xref rid="R114" ref-type="bibr">Xu and Wang 2013</xref>). However, our current simulations suggest that the lofting aerodynamics derives from a vortex ring <italic toggle="yes">shed</italic> by the decelerating disk rather than the direct impacting of the vortex ring on the wall.</p><p id="P56">A real powder consists of primary particles, aggregates, and agglomerates, held together by forces of different strengths (aggregates being more strongly bound than the larger agglomerates). None of this complexity is included in our model; in particular, we have neglected break-up processes of the agglomerates, clearly important as the agglomerate impacts the surface. We have focused on the aerodynamic source (a falling agglomerate) resuspending the smaller particles (primary particles or smaller aggregates) previously deposited on the surface. In addition, we have neglected any particle-surface interactions, which must be overcome to effect the resuspension.</p><p id="P57">The actual dust cloud generated from the splash of a real falling powder will result from contributions from a population of falling aggregates, with a distribution of sizes and arrival times. Modeling the time evolution of real dust clouds will necessitate incorporating the statistics of this impacting population of aggregates, convoluted with a distribution of arrival times.</p></sec><sec id="S18"><label>5.</label><title>Conclusion</title><p id="P58">We have studied dust generation from the splash of a falling powder on a solid surface. This has been modeled as the aerodynamic resuspension of particles from the bottom surface due to the aerodynamic back flow induced by a pellet disk impacting the bottom surface.</p><p id="P59">In the model, a layer of primary particles is loosely distributed at the bottom of the chamber. A pellet disk (which models a larger aggregate) is released and falls freely to the bottom surface under gravity. Backflow is generated by the vorticity shed from the decelerating disk; particles are suspended by this shed vorticity. We have studied the structure (dustiness profile, dust cloud profile) and dynamics (centroid trajectory) of the dust cloud. We have examined changes in the dust cloud with the size of the suspended primary particles. The model is relatively insensitive (resulting in only minor changes in the dust cloud) to changes in the structure (radius and thickness) of the falling pellet disk.</p><p id="P60">We believe that this aerodynamic resuspension mechanism is important for dust generation in a variety of industrial processes (powder pouring, spilling, and conveyor transferring). The model provides an initial attempt to calculate the structure and evolution of the dust cloud produced by such processes.</p><p id="P61">While the isolated splash process has not been utilized as a stand-alone dustiness measurement technique, a qualitative observation may be made. Given its intermediate aerodynamic strength (Re ~ 10<sup>3</sup>), the splash of falling powders is anticipated to generate more dust than the gentler rotating drum (Re ~ 10<sup>2</sup>) but less dust than the aggressive Venturi (Re ~ 10<sup>4</sup>) techniques. The present study does not yield information as to the partitioning of falling powder dust generation between the intrinsic and splash processes.</p></sec><sec sec-type="supplementary-material" id="SM1"><title>Supplementary Material</title><supplementary-material id="SD1" position="float" content-type="local-data"><label>supplemental info</label><media xlink:href="NIHMS2061031-supplement-supplemental_info.docx" id="d67e1503" position="anchor"/></supplementary-material></sec></body><back><ack id="S19"><title>Acknowledgments</title><p id="P62">We thank D. E. Evans (NIOSH) for a careful reading of the manuscript. We thank J. Bennett, K. H. Dunn, D. E. Evans (all of NIOSH), and U. Ghia (U. Cincinnati) for helpful discussions. We thank B. Alexander, D. R. and D. R. Farwick (all of NIOSH) for help with the dust cloud visualization. We thank J. C. Wells (Ritsumeikan U., Kyoto, Japan) for sharing a copy of his thesis, which documents the trajectories of individual particles lofted by Re = 25 vortex rings.</p><sec id="S20"><title>Disclaimer</title><p id="P63">The findings and conclusions of this article are those of the authors and do not necessarily represent the views of the National Institute for Occupational Safety and Health, Centers for Disease Control and Prevention. Mention of any product or company name does not constitute endorsement by the National Institute for Occupational Safety and Health, Centers for Disease Control and Prevention.</p></sec><sec id="S21"><title>Funding</title><p id="P64">This work was supported by the NIOSH Nanotechnology Research Center (NTRC project 939-0G00).</p></sec></ack><fn-group><fn id="FN1"><p id="P65"><xref rid="SD1" ref-type="supplementary-material">Supplemental data</xref> for this article is available online at <ext-link xlink:href="10.1080/02786826.2024.2417976" ext-link-type="doi">https://doi.org/10.1080/02786826.2024.2417976</ext-link></p></fn><fn fn-type="COI-statement" id="FN2"><p id="P66">Disclosure statement</p><p id="P67">No potential conflict of interest was reported by the author(s).</p></fn></fn-group><ref-list><title>References</title><ref id="R1"><mixed-citation publication-type="journal"><name><surname>Andreasen</surname><given-names>AHM</given-names></name>, <name><surname>Hofman-Bang</surname><given-names>N</given-names></name>, and <name><surname>Rasmussen</surname><given-names>NH</given-names></name>. <year>1939</year>. <article-title>&#x000dc;ber das Sta&#x000fc;bungsverm&#x000f6;ogen der Stoffe [On the ability of materials to be dusty]</article-title>. <source>Kolloid-Zeitschrift und Zeitschrift f&#x000fc;r Polymere</source>
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(b) <italic toggle="yes">t</italic>=0.3s: dust cloud resulting from the splash process.</p></caption><graphic xlink:href="nihms-2061031-f0001" position="float"/></fig><fig position="float" id="F2"><label>Figure 2.</label><caption><p id="P69">Dust generation processes in the free-falling powder: dust generation from the falling powder stream (upper part of figure); dust generation from the splash from the powder-covered surface (lower part of figure).</p></caption><graphic xlink:href="nihms-2061031-f0002" position="float"/></fig><fig position="float" id="F3"><label>Figure 3.</label><caption><p id="P70">Vertical velocity, <italic toggle="yes">v</italic><sub><italic toggle="yes">y</italic></sub>, on the central midplane (<italic toggle="yes">z</italic>=0): (a) <italic toggle="yes">t</italic>=0.5s, (b) <italic toggle="yes">t</italic>=0.6s.</p></caption><graphic xlink:href="nihms-2061031-f0003" position="float"/></fig><fig position="float" id="F4"><label>Figure 4.</label><caption><p id="P71">Out-of-plane vorticity magnitude, |<italic toggle="yes">&#x003c9;<sub>z</sub></italic>|, on the central midplane (<italic toggle="yes">z</italic>=0): (a) <italic toggle="yes">t</italic>=0.5s, (b) <italic toggle="yes">t</italic>=0.6s.</p></caption><graphic xlink:href="nihms-2061031-f0004" position="float"/></fig><fig position="float" id="F5"><label>Figure 5.</label><caption><p id="P72">Dust cloud of 1 &#x003bc;m particles (from left to right, 1, 5, 10, 15, and 20s).</p></caption><graphic xlink:href="nihms-2061031-f0005" position="float"/></fig><fig position="float" id="F6"><label>Figure 6.</label><caption><p id="P73">Trajectory of the dust cloud centroid for the standard pellet disk (<italic toggle="yes">R</italic>=4mm, <italic toggle="yes">t</italic>=3mm) falling on a monolayer of 1&#x003bc;m silica powder&#x02014;the dust cloud starts near the floor (<italic toggle="yes">r</italic>=0.026m, <italic toggle="yes">h</italic>=0.009m) at <italic toggle="yes">t</italic>=0.6s and is lofted (<italic toggle="yes">r</italic>=0.043m, <italic toggle="yes">h</italic>=0.073m) at <italic toggle="yes">t</italic>=10s.</p></caption><graphic xlink:href="nihms-2061031-f0006" position="float"/></fig><fig position="float" id="F7"><label>Figure 7.</label><caption><p id="P74">Dustiness profile&#x02014;probability of aerosolization as a function of radial distance from the impacting pellet disk.</p></caption><graphic xlink:href="nihms-2061031-f0007" position="float"/></fig><fig position="float" id="F8"><label>Figure 8.</label><caption><p id="P75">Average radius within each height slab, inverted to provide a profile of the dust cloud: <italic toggle="yes">t</italic>=1, 2.5, 5, 10, 20, 40s.</p></caption><graphic xlink:href="nihms-2061031-f0008" position="float"/></fig><fig position="float" id="F9"><label>Figure 9.</label><caption><p id="P76">Dustiness (<italic toggle="yes">t</italic>) for dust cloud lofted by the standard pellet disk (<italic toggle="yes">R</italic>=4mm, <italic toggle="yes">t</italic>=3mm) for silica powder of various diameters (particle diameter in microns shown in legend at right).</p></caption><graphic xlink:href="nihms-2061031-f0009" position="float"/></fig><fig position="float" id="F10"><label>Figure 10.</label><caption><p id="P77">Dust cloud centroid trajectory for dust clouds of different particle sizes: (a) <italic toggle="yes">d</italic>=0.5, 1, 2.5, 5 &#x003bc;m; (b) <italic toggle="yes">d</italic>=7.5, 10, 12.5&#x003bc;m; (c) <italic toggle="yes">d</italic>=15, 17.5, 20, 25&#x003bc;m.</p></caption><graphic xlink:href="nihms-2061031-f0010" position="float"/></fig><fig position="float" id="F11"><label>Figure 11.</label><caption><p id="P78">Dust cloud profile for various times (listed in legend at right) for clouds of particles of different particle sizes: (a) <italic toggle="yes">d</italic>=2.5&#x003bc;m; (b) <italic toggle="yes">d</italic>=5&#x003bc;m; (c) <italic toggle="yes">d</italic>=7.5&#x003bc;m; (d) <italic toggle="yes">d</italic>=10&#x003bc;m.</p></caption><graphic xlink:href="nihms-2061031-f0011" position="float"/></fig><fig position="float" id="F12"><label>Figure 12.</label><caption><p id="P79">Maximum diameter of suspended sediment particle (as determined by the Shields criterion) as a function of the impact velocity of the falling pellet. The vertical line (at <italic toggle="yes">v</italic>=3.64m/s) indicates the simulations of this study.</p></caption><graphic xlink:href="nihms-2061031-f0012" position="float"/></fig></floats-group></article>