Kelly Stephani

20062019
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Research Output 2006 2019

A state-resolved dsmc recombination model using orbiting cross-sections from the o3 potential energy surface

Pan, T. J., Kondur, C., Subramaniam, S. & Stephani, K., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Potential energy surfaces
Relaxation processes
Monte Carlo methods
Stabilization
Scattering

A state-resolved DSMC recombination model with orbiting-pair cross-sections

Pan, T. J., Subramaniam, S., Kondur, C. & Stephani, K., Aug 5 2019, 31st International Symposium on Rarefied Gas Dynamics, RGD 2018. Lockerby, D., Emerson, D. R., Wu, L. & Zhang, Y. (eds.). American Institute of Physics Inc., 070017. (AIP Conference Proceedings; vol. 2132).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Open Access
recombination
cross section
trajectories
cross sections
oxygen

Comparison of CFD and DSMC using calibrated transport parameters

Liechty, D. S., Wise, A. J., Subramaniam, S. & Stephani, K., Aug 5 2019, 31st International Symposium on Rarefied Gas Dynamics, RGD 2018. Lockerby, D., Emerson, D. R., Wu, L. & Zhang, Y. (eds.). American Institute of Physics Inc., 070016. (AIP Conference Proceedings; vol. 2132).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Open Access
computational fluid dynamics
fluid mechanics
multiphase flow
simulation
continuums

Computation of orbiting cross-sections from ab initio potential energy surfaces for recombination of atomic oxygen

Kondur, C., Subramaniam, S., Pan, T. J. & Stephani, K., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Potential energy surfaces
Oxygen
Atoms
Trajectories
Scattering

Computation of state to state transport coefficients using ab initio potential energy surfaces for the o + o2 system

Subramaniam, S. & Stephani, K., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Potential energy surfaces
Thermal conductivity
Viscosity
Reentry
Hypersonic aerodynamics

Honors & Recognition

air force
basic research
engineering
science
engineer