Comparison of approximate analytical and numerical solutions for heat fluxes in viscous supersonic flow past a body

DOI10.1007/BF02230754zbMath0870.76032MaRDI QIDQ1354791

I. G. Brykina, V. I. Sakharov

Publication date: 22 September 1997

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

zbMATH Keywords

spheresellipsoidsstagnation pointpressure distributionblunt bodyparaboloidscomplete Navier-Stokes equationsviscous perfect gas

Mathematics Subject Classification ID

Supersonic flows (76J20)

Related Items (2)

Approximate analytical solutions for heat fluxes in three-dimensional hypersonic flow over blunt bodies ⋮ Аналитическое исследование ламинарного пограничного слоя около затупленных тел

Cites Work

• Unnamed Item
• Approximate formulas for heat flows towards an ideally catalytic surface near a plane of symmetry
• Approximate formulas for the heat fluxes to the surface of three- dimensional bodies
• A high-accuracy version of Godunov's implicit scheme for integrating the Navier-Stokes equations
• Integration of hypersonic viscous shock layer equations by a successive approximation method

This page was built for publication: Comparison of approximate analytical and numerical solutions for heat fluxes in viscous supersonic flow past a body