Isolator-combustor interactions in a circular model scramjet with thermal and non-thermal choking-induced unstart

DOI10.1017/JFM.2021.238zbMath1493.76119OpenAlexW3159801248MaRDI QIDQ4987905

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Publication date: 11 May 2021

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/jfm.2021.238

zbMATH Keywords

experimental verificationacoustic forcingshock-boundary layer interactionhigh-enthalpy hypersonic flowisolator shock train

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Shock waves and blast waves in fluid mechanics (76L05) Combustion (80A25) Reaction effects in flows (76V05) Hypersonic flows (76K05)

Related Items (1)

Analysis of the choking condition of one-dimensional diabatic flows with wall friction

Cites Work

• Transverse jets and jet flames. Part 1. Scaling laws for strong transverse jets
• Ignition, flame structure and near-wall burning in transverse hydrogen jets in supersonic crossflow
• Unstart phenomena induced by mass addition and heat release in a model scramjet
• On the origin and propagation of perturbations that cause shock train inherent unsteadiness
• Transient fluid-combustion phenomena in a model scramjet

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