Implementation of a Chemical Kinetics Model for Hypersonic Flows in Air for High-Performance CFD-Reference-Cited by-同舟云学术

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Implementation of a Chemical Kinetics Model for Hypersonic Flows in Air for High-Performance CFD

Published:2020-01-05 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2020 Forum
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Author:

Chaudhry Ross S.¹,Boyd Iain D.¹,Torres Erik²,Schwartzentruber Thomas E.²,Candler Graham V.²

Affiliation:

1. University of Michigan, Ann Arbor

2. University of Minnesota, Minneapolis

Publisher

American Institute of Aeronautics and Astronautics

Reference39 articles.

1. Nonequilibrium Hypersonic Aerothermodynamics

2. Reactive Scattering Cross Sections III: Quasiclassical and Semiclassical Methods

3. State-resolved master equation analysis of thermochemical nonequilibrium of nitrogen

4. Rovibrational energy transfer and dissociation in O2–O collisions

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1. Shock-Layer Measurements in T5 Shock Tunnel Hypersonic Flows Around a Cylinder Model;AIAA Journal;2024-08-23

2. High-Temperature Nonequilibrium Air Chemistry from First Principles;Journal of Thermophysics and Heat Transfer;2024-04

3. Discontinuous Galerkin methods for hypersonic flows;Progress in Aerospace Sciences;2024-04

4. How much does thermal nonequilibrium influence the overall atomic recombination during de-excitation?;Chemical Physics;2024-04

5. Vibrational-State-Resolved Oxygen and Nitric Oxide Time-History Measurements in Shock-Heated, High-Temperature Air;AIAA SCITECH 2024 Forum;2024-01-04

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