Rate-dependent energetic processes in hypersonic flows

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Abstract

In celebration of the first 60 years of the Air Force Office of Scientific Research, several studies of hypersonic flows dominated by rate-dependent energetic processes are revisited. The work presented shows the evolution and advancement of computational capabilities in this area, and illustrates some key lessons learned over the previous decade or so. Early work with Leyva and Hornung in the California Institute of Technology T5 Free-Piston Shock Tunnel had the goal of validating thermochemical models for high-enthalpy flows. Several of these flows are re-analyzed with more advanced numerical methods, resulting in improved comparisons with the experimental measurements. This work was followed by a series of experiments in the Calspan-University at Buffalo Research Center (now CUBRC Inc.) facilities at lower enthalpy conditions. Initial comparisons were poor, but with a better understanding of the facility behavior and the inclusion of key finite-rate processes, excellent agreement was obtained for nitrogen flows. An interesting study related to plasmadynamics and finite-rate processes in a different type of flow is discussed. Finally, it is shown that recent advances in numerical methods that are beginning to enable the direct numerical simulation of key rate-dependent energetic processes in hypersonic flows.

Original languageEnglish (US)
Pages (from-to)37-48
Number of pages12
JournalProgress in Aerospace Sciences
Volume72
DOIs
StatePublished - Jan 1 2015

Bibliographical note

Funding Information:
This work was sponsored by the Air Force Office of Scientific Research under grants FA9550-10-1-0563 and FA9550-12-1-0064 and by the Department of Defense National Security Science & Engineering Faculty Fellowship . The views and conclusions contained herein are those of the author and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of the AFOSR or the U.S. Government.

Publisher Copyright:
© 2014 Elsevier Ltd. All rights reserved.

Keywords

  • Computational fluid dynamics
  • Hypersonics
  • Nonequilibrium

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