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TGQR 2010Q4 Report.pdf - Teragridforum.org

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In 2010, Aidun and colleagues made use of TeraGrid resources at Purdue, LONI, NCSA and<br />

TACC. The researchers have examined exceedingly complex noncolloidal suspensions, work<br />

which lends itself to varied applications such as biological systems (blood flow), paper<br />

manufacturing (wood fiber and coating flows), mining and petroleum industries (for waste<br />

trailing), and home products (paint and cosmetics). For example, blood is comprised of elements<br />

such as red blood cells and platelets suspended in plasma. Most computational modeling of blood<br />

flow has simplified blood as pure fluid flow without the presence of actual suspended particles.<br />

Understanding the physics of blood flow requires accurate simulation of the suspended solid<br />

particles to capture the suspension structure and the blood elements on a microscale. This kind of<br />

understanding could be important in, among other things, treating pathological blood clots, a<br />

common cause of heart attacks and strokes, which strike more than 2 million Americans annually.<br />

Clot formation and detachment also plays into such medical issues as the failure of popular<br />

bileaflet mechanical heart valves. Aidun’s group published results from such simulations more<br />

than once in 2010, including “Parallel Performance of a Lattice-Boltzmann/Finite Element<br />

Cellular Blood Flow Solver on the IBM Blue Gene/P Architecture,” Computer Physics<br />

Communications, 181:1013-1020, 2010. Their paper “Numerical Investigation of the Effects of<br />

Channel Geometry on Platelet Activation and Blood Damage,” accepted by Annals of Biomedical<br />

Engineering in October 2010, reports results that may help optimize the design of prosthetic<br />

replacement heart valves. The researchers also are looking at extremely complex flows through<br />

saturated deformable media, work that could provide insight into material properties of foams and<br />

felts used in industrial applications and lead to improvement in the designs of these materials.<br />

2.2.13<br />

Fluid, Particulate, and Hydraulic Systems: Large Eddy Simulation Investigations of<br />

Aviation Environmental Impacts (PI: Sanjiva Lele, Stanford)<br />

One of the impacts about which the climate research community is very uncertain is the extent to<br />

which aircraft change cloud cover. That’s why Sanjiva Lele and his team at Stanford University,<br />

including PhD candidate Alexander Naiman, are studying the impact of commercial aviation on<br />

global climate. The direct effect is known: that airplanes produce<br />

contrails, which are clouds of ice particles, under certain atmospheric<br />

conditions. But Lele and Naiman have shown there’s also an indirect<br />

effect, where jet contrails induce cirrus cloud formation where clouds<br />

might not have formed naturally otherwise. This is a concern, as<br />

increased cloud cover may reduce a region’s temperature as well as<br />

the amount of solar energy a region receives.<br />

The portion of the research that's being conducted on Abe at NCSA is<br />

a Large Eddy Simulation (LES) of contrails using a highly scalable<br />

parallelized LES code that was developed at Stanford. It is a new<br />

model of aircraft exhaust plume dilution that is used as a subgrid scale<br />

model within a large-scale atmospheric simulation, providing<br />

predictive equations for the evolution of individual exhaust plumes<br />

based on parameters provided by the large-scale simulation. The<br />

simulations start with the wake of a commercial airliner at a cruise<br />

condition, one second after the airplane has passed. In addition to<br />

solving the LES fluid equations, they also compute the deposition of<br />

water vapor onto the ice particles that form a contrail, leading to<br />

cirrus cloud formation. The outputs of their simulations include 3D<br />

fields of all the simulation variables at certain time intervals, which<br />

was not previously possible.<br />

Current simulations continue for 1200 seconds (20 minutes), and the<br />

Figure 2.13. This image shows 3D<br />

isosurfaces of two quantities. The<br />

opaque surfaces on the inside are<br />

vorticity magnitude colored by<br />

streamwise vorticity; these show the<br />

development of the aircraft wake<br />

vortices, which are what give contrails<br />

interesting dynamics. The vortices are<br />

initially parallel, then they form loops<br />

and interact chaotically until they<br />

dissipate. The translucent green/blue<br />

outer surface shows the aircraft jet<br />

exhaust scalar, which essentially<br />

defines the outer extent of the contrail.<br />

21

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