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We gratefully acknowledge funding for this research provided by the National Science Foundation, NASA, AFOSR, DOE, Air Force Research Laboratory and the University of Illinois at Urbana-Champaign.

 

Computational resources and technical support are provided by NASA through the High-End Computing Capability (HECC) and by DOE through the PSAAP Center.

research activities

hybrid continuum/kinetic solver for chemically reacting flows

 

combined kinetic approach for DSMC rare events and tail-driven processes
assessment of continuum breakdown in high-speed chemically reacting flows
exploiting the role of defects for enhanced thermoelectric material performance
calibration of DSMC parameters for transport processes in ionized air based on ab initio calculations

The computational kinetics group employs DSMC, deterministic Boltzmann methods and MD to explore and improve modeling for engineering systems ranging from high-altitude, rarefied flows to material modification and material response through irradiation processing.

 

 

Some of our current research activities include:

The careful treatment of transport properties is of paramount importance to ensure consistency between computational transport models employed in flow solvers, from deterministic methods to stochastic, particle-based methods. Such considerations are important when comparing flowfield solutions between, for example, computational fluid dynamics (CFD) and direct simulation Monte Carlo (DSMC) methods, but consistency is especially critical for use of these methods within hybrid CFD/DSMC frameworks. Simply stated, the same material at the same conditions, should have the same properties where both CFD and DSMC flow solutions are applicable. In the context of hybrid solutions, this ensures that the same flow problem is being solved by each method and the differences between the solutions are due to fundamental non-equilibrium processes, rather than differences in the physical models. The DSMC collision cross section model parameters are calibrated for high temperature atmospheric conditions
DSMC study of carbon fiber oxidation in ablative thermal protection systems

The careful treatment of transport properties is of paramount importance to ensure consistency between computational transport models employed in flow solvers, from deterministic methods to stochastic, particle-based methods. The DSMC collision cross section model parameters are calibrated for high temperature atmospheric conditions by matching the collision integrals from DSMC against ab initio based collision integrals. The DSMC parameter values are computed for the widely used Variable Hard Sphere (VHS) and the Variable Soft Sphere (VSS) models using the collision-average and collision-specific pairing approaches. The recommended model parameter values can be readily applied to any gas mixture involving binary collisional interactions between the chemical species presented for the specified temperature range.

Calibration of DSMC parameters for transport processes in ionized air based on ab initio calculations

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