Approximate formulas for heat flows towards an ideally catalytic surface near a plane of symmetry

DOI10.1016/0021-8928(89)90082-8zbMath0734.76081OpenAlexW2083199910MaRDI QIDQ811288

V. V. Rusakov, V. G. Shcherbak, I. G. Brykina

Publication date: 1989

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(89)90082-8

zbMATH Keywords

angle of attackheat fluxthree-dimensional flowsuccessive approximationsnumerical computationsideally catalytic surfaceplane of symmetryblunt bodieschemically unstable viscous gasthin, viscous shock layer

Mathematics Subject Classification ID

Reaction effects in flows (76V05) Supersonic flows (76J20)

Related Items (5)

Comparison of approximate analytical and numerical solutions for heat fluxes in viscous supersonic flow past a body ⋮ Approximate analytical solutions for heat fluxes in three-dimensional hypersonic flow over blunt bodies ⋮ Heat transfer to blunt-edged swept wings at angle of attack in hypersonic flow ⋮ Approximate formulas for the heat fluxes to the surface of three- dimensional bodies ⋮ Approximate formulas for heat flows towards an ideally catalytic surface near a plane of symmetry

Cites Work

• Unnamed Item
• Approximate formulas for heat flows towards an ideally catalytic surface near a plane of symmetry
• Investigation of hypersonic three-dimensional flow past blunt bodies within the framework of the parabolized Navier-Stokes equations
• Three-dimensional laminar boundary layer on a permeable surface in the neighborhood of a symmetry plane
• Integration of hypersonic viscous shock layer equations by a successive approximation method
• Reacting Shock Layers with Slip and Catalytic Boundary Conditions

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