Design of the supersonic part of a maximum thrust spatial nozzle

DOI10.1134/S0965542521100109zbMath1493.76081OpenAlexW3212715985MaRDI QIDQ2245896

I. E. Mikhailov

Publication date: 15 November 2021

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

Full work available at URL: https://doi.org/10.1134/s0965542521100109

zbMATH Keywords

necessary optimality conditionLagrange multiplier methoditerative numerical methodLagrange functionalcircular critical cross-section

Mathematics Subject Classification ID

Variational methods applied to problems in fluid mechanics (76M30) Supersonic flows (76J20) Flow control and optimization for compressible fluids and gas dynamics (76N25) Basic methods in fluid mechanics (76M99)

Cites Work

• Unnamed Item
• Contouring optimal three-dimensional nozzles
• The optimization of the supersonic parts of three-dimensional nozzles
• The method of characteristics for calculating three-dimensional supersonic irrotational flows

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