Approximate formulas for the heat fluxes to the surface of three- dimensional bodies

DOI10.1016/0021-8928(92)90011-VzbMath0787.76039OpenAlexW2086703864MaRDI QIDQ1314205

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

Publication date: 7 March 1994

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(92)90011-v

zbMATH Keywords

stagnation pointperfect gashypersonic viscous shock layerblunt bodiesgeometrical characteristicsintegral method of successive approximations

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Related Items (1)

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

Cites Work

• Investigation of three-dimensional boundary layers on blunt bodies with permeable surface
• Approximate formulas for heat flows towards an ideally catalytic surface near a plane of symmetry
• Numerical study of three-dimensional boundary layer in a compressible gas
• Unnamed Item
• Unnamed Item
• Unnamed Item

This page was built for publication: Approximate formulas for the heat fluxes to the surface of three- dimensional bodies