The optimization of the supersonic parts of three-dimensional nozzles

DOI10.1016/0041-5553(81)90028-8zbMath0527.76052OpenAlexW2072868183MaRDI QIDQ3042714

I. E. Mikhajlov, V. M. Borisov

Publication date: 1981

Published in: USSR Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0041-5553(81)90028-8

zbMATH Keywords

method of characteristicsaxial symmetryextremal thrust nozzle designing

Mathematics Subject Classification ID

Gas dynamics (general theory) (76N15) Supersonic flows (76J20) Basic methods in fluid mechanics (76M99)

Related Items (2)

Contouring optimal three-dimensional nozzles ⋮ Design of the supersonic part of a maximum thrust spatial nozzle

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