Aerodynamic response of internal passages to pulsating inlet supersonic conditions

DOI10.1016/J.COMPFLUID.2017.03.005zbMath1390.76222OpenAlexW2592403449WikidataQ59197956 ScholiaQ59197956MaRDI QIDQ1648228

Jorge Saavedra, Guillermo Paniagua, Jorge Pinho de Sousa

Publication date: 27 June 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2017.03.005

zbMATH Keywords

hysteresiswave propagationunsteady flowcharacteristic waveswave modulationsupersonic passages

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Direct numerical and large eddy simulation of turbulence (76F65) Supersonic flows (76J20)

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Cites Work

• Computational and experimental investigation into aerodynamic interference between slender bodies in supersonic flow
• Influence of numerical and viscous dissipation on shock wave reflections in supersonic steady flows.
• A numerical study of a converging cylindrical shock
• On the transient response of the turbulent boundary layer inception in compressible flows

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