State-Resolved Aerothermodynamic Modeling for Air Using QCT Data

Abstract

Recently, due to continued advancements in computational chemistry and large-scale parallel computing, molecular level physics can be investigated using ab-initio computations. The most common analysis technique is called Quasi-Classical-Trajectory (QCT) analysis, wherein a large number of individual molecular collisions are simulated using a potential energy surface (PES) that dictates the forces on individual atoms comprising the molecules. Since the molecular systems of interest for air are small (typically 2-4 atoms), the PES can be fit to highly accurate electronic structure calculations. In the past 5 years a number of such results have been reported. The challenge now is to reduce this huge amount of data into accurate, yet tractable, models for predictive hypersonic flow simulations. The goal of the grant research was to develop accurate, yet tractable, models for both the direct simulation Monte Carlo (DSMC) particle method as well as for continuum computational fluid dynamics (CFD) methods.

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Document Details

Document Type
Technical Report
Publication Date
Dec 20, 2018
Accession Number
AD1090770

Entities

People

  • Thomas E. Schwartzentruber

Organizations

  • Regents of the University of Minnesota

Tags

DTIC Thesaurus Topics

  • Air Force
  • Air Force Research Laboratories
  • Chemistry
  • Collisions
  • Computational Chemistry
  • Computational Fluid Dynamics
  • Energy
  • Fluid Dynamics
  • Governments
  • Hypersonic Flow
  • Molecules
  • Monte Carlo Method
  • Particles
  • Physical Chemistry
  • Potential Energy
  • Simulations
  • Trajectories

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Computational Modeling and Simulation
  • Molecular Photonics/Laser Physics

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Microelectronics