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Thomas E. Schwartzentruber

Researcher at University of Minnesota

Publications -  165
Citations -  3272

Thomas E. Schwartzentruber is an academic researcher from University of Minnesota. The author has contributed to research in topics: Direct simulation Monte Carlo & Dissociation (chemistry). The author has an hindex of 29, co-authored 145 publications receiving 2554 citations. Previous affiliations of Thomas E. Schwartzentruber include University of Toronto & University of Michigan.

Papers
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An improved potential energy surface and multi-temperature quasiclassical trajectory calculations of N2 + N2 dissociation reactions

TL;DR: As T(v) decreases, rotational energy appears to compensate for the decline in average vibrational energy in promoting dissociation, and the dissociation probability's dependence on v weakens.
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A hybrid particle-continuum method applied to shock waves

TL;DR: A hybrid numerical scheme designed for hypersonic non-equilibrium flows is presented which solves the Navier-Stokes equations in regions of near-equ equilibrium and uses the direct simulation Monte Carlo method where the flow is in non-Equilibrium.
Journal ArticleDOI

A modular particle-continuum numerical method for hypersonic non-equilibrium gas flows

TL;DR: A modular particle-continuum (MPC) numerical method for steady-state flows is presented which solves the Navier-Stokes equations in regions of near-equ equilibrium and uses the direct simulation Monte Carlo (DSMC) method to simulate regions of non-equilibrium gas flow.
Journal ArticleDOI

Direct molecular simulation of nitrogen dissociation based on an ab initio potential energy surface

TL;DR: In this article, a direct molecular simulation (DMS) approach is used to predict the internal energy relaxation and dissociation dynamics of high-temperature nitrogen molecules by providing forces between the four atoms.
Book

Nonequilibrium Gas Dynamics and Molecular Simulation

TL;DR: In this paper, the authors provide an updated treatment of molecular gas dynamics topics for aerospace engineers, or anyone researching high-temperature gas flows for hypersonic vehicles and propulsion systems.