Investigation of shock dynamics in an axisymmetric inlet/isolator with attached boundary layers

DOI10.1017/JFM.2020.899zbMath1461.76390OpenAlexW3111765931MaRDI QIDQ5145034

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Publication date: 19 January 2021

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

Full work available at URL: https://doi.org/10.1017/jfm.2020.899

zbMATH Keywords

shock wavescompressible boundary layershigh-speed flow

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

• Unnamed Item
• Unsteady shock wave dynamics
• Experimental evidence for Plotkin model of shock unsteadiness in separated flow
• On the origin and propagation of perturbations that cause shock train inherent unsteadiness
• Analysis and modelling of unsteady shock train motions

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