On the theory of separation of a laminar boundary layer in a supersonic flow

DOI10.1007/BF01091076zbMath0563.76062OpenAlexW1997993908MaRDI QIDQ1057734

I. I. Lipatov

Publication date: 1984

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01091076

zbMATH Keywords

laminar boundary layerviscous gasadverse pressure gradientelimination of the singularity

Mathematics Subject Classification ID

Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (1)

Interaction and separation in internal flows with low skin friction

Cites Work

• Asymptotic theory of short separation regions on the leading edge of a slender airfoil
• Self-induced separation
• Is the singularity at separation removable?
• ON LAMINAR BOUNDARY-LAYER FLOW NEAR A POSITION OF SEPARATION
• On boundary layers and upstream influence. I. A comparison between subsonic and supersonic flows

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