Effect of large blowing rates on the compressible boundary layer flow at the stagnation point of a rotating sphere
type: Item
instance of: scholarly article
title: Effect of large blowing rates on the compressible boundary layer flow at the stagnation point of a rotating sphere
zbMATH Open document ID: 0881.76081
DOI: 10.1007/BF01262526
author: M. Kumari
author: G. Nath
published in: Acta Mechanica
publication date: 1998-02-25T00:00:00Z
review text: The effect of a large surface blowing (injection) rate on the steady laminar compressible boundary-layer flow at the forward stagnation point of a rotating sphere has been studied. The resulting coupled nonlinear ordinary differential equations have been solved using two methods, namely, the method of matched asymptotic expansion and the implicit finite difference scheme in combination with the quasilinearization technique.
Mathematics Subject Classification ID: 76N20
Mathematics Subject Classification ID: 76U05
Mathematics Subject Classification ID: 76M20
zbMATH DE Number: 1019275
zbMATH Keywords: boundary layer thickness
zbMATH Keywords: longitudinal shear stress
zbMATH Keywords: total enthalpy
zbMATH Keywords: rotation parameters
zbMATH Keywords: method of matched asymptotic expansion
zbMATH Keywords: implicit finite difference scheme
zbMATH Keywords: quasilinearization technique
MaRDI profile type: Publication
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cites work: Laminar flow at a three-dimensional stagnation point with large rates of injection
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full work available at URL: https://doi.org/10.1007/bf01262526
OpenAlex ID: W1986182340
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description: scientific article; zbMATH DE number 1019275