Abstract. Detailed simulations were performed with a continuum-based Navier-Stokes, a gas kinetic Bhatnagar-Gross-Krook (BGK) and the Direct Simulation Monte Carlo (DSMC) flow solvers to identify and characterize the translational and internal energy mode relaxation in high speed flows. Argon and nitrogen shock structures were simulated to quantify the nonequilibrium state. A new multi-translational temperature gas kinetic model was developed to match the capability of DSMC. Bulk viscosity as an adjustable parameter to recover small departures from rotational equilibrium in the Navier-Stokes equations is explored in weak shock structures. In the context of nitrogen dissociation, the models of vibrational bias for the dissociation kinetics a...
University of Minnesota Ph.D. dissertation. November 2018. Major: Aerospace Engineering and Mechanic...
A gas-kinetic model with multiple translational temperature for the continuum and near continuum flo...
Accurately computing the inner structure of normal shock waves or oblique shock waves is crucial for...
Numerical simulations are presented of steady state, hypersonic blunt body nitrogen flow for conditi...
University of Minnesota Ph.D. dissertation. August 2013. Major: Aerospace Engineering and Mechanics....
It is well known that for increasingly rarefied flowfields, the predictions from continuum formulati...
Numerical simulations of high-speed, high-altitude flow over re-entry objects have been carried out ...
Are extensions to continuum formulations for solving fluid dynamic problems in the transition-to-rar...
International audienceFour different types of macroscopic models developed for the vibration-chemist...
This paper reports some preliminary progress in developing a gaskinetic Computational Fluid Dynamic ...
Fully kinetic, vibrationally kinetic, and continuum solvers with varying model fidelity are used in ...
There has been a continuous effort to unveil the physics of hypersonic flows both experimentally and...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90705/1/AIAA-2011-448-920.pd
As a hypersonic vehicle travels through the atmosphere, it crosses many flow regimes, from rarefied ...
Includes bibliographical references (pages 76-77)Numerical simulations of non-continuum gas flows ar...
University of Minnesota Ph.D. dissertation. November 2018. Major: Aerospace Engineering and Mechanic...
A gas-kinetic model with multiple translational temperature for the continuum and near continuum flo...
Accurately computing the inner structure of normal shock waves or oblique shock waves is crucial for...
Numerical simulations are presented of steady state, hypersonic blunt body nitrogen flow for conditi...
University of Minnesota Ph.D. dissertation. August 2013. Major: Aerospace Engineering and Mechanics....
It is well known that for increasingly rarefied flowfields, the predictions from continuum formulati...
Numerical simulations of high-speed, high-altitude flow over re-entry objects have been carried out ...
Are extensions to continuum formulations for solving fluid dynamic problems in the transition-to-rar...
International audienceFour different types of macroscopic models developed for the vibration-chemist...
This paper reports some preliminary progress in developing a gaskinetic Computational Fluid Dynamic ...
Fully kinetic, vibrationally kinetic, and continuum solvers with varying model fidelity are used in ...
There has been a continuous effort to unveil the physics of hypersonic flows both experimentally and...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90705/1/AIAA-2011-448-920.pd
As a hypersonic vehicle travels through the atmosphere, it crosses many flow regimes, from rarefied ...
Includes bibliographical references (pages 76-77)Numerical simulations of non-continuum gas flows ar...
University of Minnesota Ph.D. dissertation. November 2018. Major: Aerospace Engineering and Mechanic...
A gas-kinetic model with multiple translational temperature for the continuum and near continuum flo...
Accurately computing the inner structure of normal shock waves or oblique shock waves is crucial for...