Influence of second-order boundary layer effects in hypersonic flow over slender blunt cones

DOI10.1007/BF01051333zbMATH Open0789.76060OpenAlexW2088450545MaRDI QIDQ1317754

M. O. Fridlender, G. A. Tirskiy, D. Kh. Gan'zha, Sergei V. Utyuzhnikov

Publication date: 12 April 1994

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

Full work available at URL: https://doi.org/10.1007/bf01051333

zbMATH Keywords

Euler equationscomplete viscous shock layer equationsentropy layer absorption

Mathematics Subject Classification ID

Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

• Title not available (Why is that?)

Related Items (2)

Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack ⋮ Laminar base flow downstream of slender cones in hypersonic flow

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