FREELY INTERACTING AXISYMMETRIC BOUNDARY LAYERS ON BODIES OF REVOLUTION

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DOI10.1093/qjmam/38.4.575zbMath0581.76071OpenAlexW2093654551MaRDI QIDQ3703496

Alfred Kluwick, Philipp Gittler, R. J. Bodonyi

Publication date: 1985

Published in: The Quarterly Journal of Mechanics and Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1093/qjmam/38.4.575

zbMATH Keywords

singularity separation point two-dimensional flows Analytical expressions plateau region uniform supersonic flow expansive free interactions freely interacting laminar axisymmetric boundary layers solutions for compressive free interactions triple-deck flow structure

Mathematics Subject Classification ID

Supersonic flows (76J20) Basic methods in fluid mechanics (76M99)

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A numerical method for treating strongly interactive three-dimensional viscous-inviscid flows, Global stability of supersonic flow over a hollow cylinder/flare, An investigation of transonic flow over axisymmetric rigid body

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