Modeling of a Reduced Hybrid H<sub>2</sub>–Air Kinetic Scheme Integrating the Effect of Hypersonic Reactive Air with Supersonic Combustion

Modeling of a Reduced Hybrid H<sub>2</sub>–Air Kinetic Scheme Integrating the Effect of Hypersonic Reactive Air with Supersonic Combustion

A hybrid H<sub>2</sub>–air kinetic scheme of 11 species and 15 reactions is developed, which is capable of simulating the high-temperature air reaction flows and H<sub>2</sub>–O<sub>2</sub> combustion flows respectively or simultaneously. Based on the Gupta scheme...

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Autores principales: Longfei Li, Jiangfeng Wang
Formato: article
Lenguaje:EN
Publicado: MDPI AG 2021
Materias:
hypersonic reactive flow
H<sub>2</sub>–O<sub>2</sub> combustion reactions
sensitivity analysis
ignition delay time
shock-induced detonation
kinetic scheme
Technology
T
Acceso en línea:https://doaj.org/article/923a55e5bac544e7904af57a28023546
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