Numerical investigation of supersonic viscous gas flow over long blunt cones with allowance for equilibrium physicochemical effects

DOI10.1007/BF01055655zbMath0789.76058OpenAlexW4210283957WikidataQ122469127 ScholiaQ122469127MaRDI QIDQ1317818

V. Pereyra

Publication date: 12 April 1994

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

Full work available at URL: https://doi.org/10.1007/bf01055655

zbMATH Keywords

viscous shock layer equationsaxisymmetric heat-conducting gas flowglobal iterationsheat loadssecond-approximation effects of boundary layer theory

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Reaction effects in flows (76V05) Supersonic flows (76J20)

Related Items (1)

Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence

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