On the theory of separation of a laminar boundary layer in a supersonic flow
type: Item
instance of: scholarly article
title: On the theory of separation of a laminar boundary layer in a supersonic flow
zbMATH Open document ID: 0563.76062
DOI: 10.1007/BF01091076
author: I. I. Lipatov
published in: Fluid Dynamics
publication date: 1984-01-01T00:00:00Z
review text: In the present paper, we propose a flow model that permits elimination of the singularity at the point of separation of the laminar boundary layer in a supersonic flow in the case of a given adverse pressure gradient.
Mathematics Subject Classification ID: 76J20
Mathematics Subject Classification ID: 76N20
zbMATH DE Number: 3898470
zbMATH Keywords: viscous gas
zbMATH Keywords: elimination of the singularity
zbMATH Keywords: laminar boundary layer
zbMATH Keywords: adverse pressure gradient
MaRDI profile type: Publication
cites work: ON LAMINAR BOUNDARY-LAYER FLOW NEAR A POSITION OF SEPARATION
cites work: Self-induced separation
cites work: Is the singularity at separation removable?
cites work: On boundary layers and upstream influence. I. A comparison between subsonic and supersonic flows
cites work: Asymptotic theory of short separation regions on the leading edge of a slender airfoil
full work available at URL: https://doi.org/10.1007/bf01091076
OpenAlex ID: W1997993908
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description: scientific article; zbMATH DE number 3898470