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Scientific and Technical Aerospace Reports Volume 39 April 6, 2001

Scientific and Technical Aerospace Reports Volume 39 April 6, 2001

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surprising findings of these studies are that superfluid droplets are ”sticky” in the sense that they exhibit an anomalously large<br />

contact angle hysteresis, <strong>and</strong> that superfluid drops require a substantial force to initiate flow. Despite the very low viscosity, the<br />

drops have a mechanical Q factor similar to water. We are in the process of developing a next generation 3-He based optical cryostat<br />

that will allow us to extend our studies to lower temperatures. We plan to study superfluid spreading on a dry wettable surface,<br />

which requires a cesium dam to form a dry spot. Temperatures below 0.3K are required to eliminate vapor phase mass transport.<br />

We will also study the mechanical Q of drops in the limit of zero vapor pressure <strong>and</strong> unity superfluid fraction. The dynamics of<br />

dewetting <strong>and</strong> film rupture can be studied by forming metastable films of superfluid on a substrate whose thermodynamically<br />

stable state is dry.<br />

Author (revised)<br />

Liquid-Solid Interfaces; Superfluidity; Liquid Helium; Wetting; Wettability<br />

<strong>2001</strong>0024985 National Center for Microgravity Research on Fluids <strong>and</strong> Combusiton, Clevel<strong>and</strong>, OH USA<br />

Splashing Droplets<br />

V<strong>and</strong>erWal, R. L., National Center for Microgravity Research on Fluids <strong>and</strong> Combusiton, USA; Tryggvason, Gretar, Michigan<br />

Univ., USA; Kizito, John P., National Center for Microgravity Research on Fluids <strong>and</strong> Combusiton, USA; Alex<strong>and</strong>er, Iwan, Case<br />

Western Reserve Univ., USA; Proceedings of the Fifth Microgravity Fluid Physics <strong>and</strong> Transport Phenomena Conference; December<br />

2000, pp. 1<strong>39</strong>5-1<strong>39</strong>6; In English; See also <strong>2001</strong>0024890; No Copyright; Abstract Only; Available from CASI only as part<br />

of the entire parent document<br />

In practical applications involving sprays for cooling, atomization, coating <strong>and</strong> fuel injection, the small spatial scales <strong>and</strong><br />

short temporal scales prohibit detailed study of the internal fluid dynamics <strong>and</strong> surface <strong>and</strong> internal temperature profile during<br />

the droplet-surface interaction. Such information is critical to defining ranges of behavior, testing existing models of droplet-wall<br />

interactions <strong>and</strong> providing benchmark data for development of theoretical models. In a low-gravity environment, enhanced spatial<br />

<strong>and</strong> temporal scales may be achieved while maintaining comparable ranges of surface tension, viscous <strong>and</strong> inertial effects, typical<br />

of practical applications with well-defined initial conditions uninfluenced by gravity. The relative magnitude of surface tension<br />

<strong>and</strong> viscosity effects will depend upon the kinematics of the impaction process, liquid properties <strong>and</strong> ambient conditions. Experiments<br />

in both the film evaporation <strong>and</strong> film boiling regimes will be conducted to illuminate surface tension gradient <strong>and</strong> viscosity<br />

effects upon droplet breakup. Parameters that will be varied include the initial bulk liquid surface tension, viscosity, degree of<br />

liquid subcooling, impact Weber number, ambient pressure <strong>and</strong> impact angle. Comparison between results will be used to delineate<br />

the role <strong>and</strong> quantify the relative magnitude of surface tension effects compared with inertial, viscous <strong>and</strong> wetting contributions<br />

to droplet breakup or ”splashing”. A second thrust of the work proposed here will be to test equivalent dimensionless groups:<br />

for example, for droplets of different size, adjustment of velocity, surface tension <strong>and</strong> viscosity will be used to equalize Weber<br />

<strong>and</strong> Reynolds numbers to test for hidden property dependencies. These tests will be used to evaluate the applicability of droplet<br />

breakup studies using widely different conditions. Experiments in the film evaporation region will provide tests of theory apart<br />

from phase change while including wetting behavior <strong>and</strong> contact angle effects. Experiments in the film boiling regime will include<br />

phase change effects while eliminating surface wetting <strong>and</strong> contact angle effects. Experiments in the nucleate <strong>and</strong> transition boiling<br />

regimes will determine whether splashing can occur prior to droplet disruption by boiling <strong>and</strong> serve to identify alternative<br />

droplet breakup behavior. The experimental data is expected to serve as input to practical spray models while detailed numerical<br />

modelling will be developed by comparison to experimental results. The experimental studies will be complemented by detailed<br />

simulation of the drop collision with the walls. A so-called on-fluid formulation will be used where a single set of equations is<br />

written for all the phases involved. In this approach the phase boundary is treated as an imbedded interface by adding the appropriate<br />

source terms to the conservation laws. These source terms are in the form of delta functions localized at the interface <strong>and</strong> are<br />

selected in such a way to satisfy the correct matching conditions at the phase boundary. More specifically, the head-on impact of<br />

a drop on a hot surface will be simulated using an axisymmetric numerical model. The model will include local grid refinement<br />

to capture the draining of the film between the drop <strong>and</strong> the surface, the energy equation to compute the temperature distribution,<br />

temperature dependent surface tension, <strong>and</strong> mass transfer from the surface due to evaporation. For the case of drops colliding with<br />

solid walls where no slip boundary conditions must be enforced, quantitative predictions will require very fine resolution. The<br />

simulations will be set up to mimic the experimental setup as closely as possible <strong>and</strong> detailed comparisons will be made. by turning<br />

various physical properties on <strong>and</strong> off <strong>and</strong> examining the sensitivity of the results to changes in the modeling of the relation<br />

between the surface tension <strong>and</strong> the temperature, for example, it will be possible to determine exactly what forces are important<br />

during the collision of drop with a hot surface <strong>and</strong> the evolution of splashed products.<br />

Author (revised)<br />

Drops (Liquids); Interfacial Tension; Computerized Simulation; Dimensionless Numbers; Splashing<br />

122

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