On the determination of the shape of a supersonic nozzle taking into consideration the variation of aircraft flight conditions

DOI10.1016/0021-8928(70)90164-4zbMath0223.76047OpenAlexW1669233654MaRDI QIDQ2548209

A. N. Krajko, Alexander A. Osipov

Publication date: 1970

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(70)90164-4

Mathematics Subject Classification ID

Supersonic flows (76J20)

Related Items (1)

Solution of the variational problem of constructing the contour of a compound nozzle

Cites Work

• On maximum thrust nozzles with arbitrary isoperimetric conditions
• Variational problems of gas dynamics of nonequilibrium and equilibrium flows
• On the solution of variational problems of supersonic flows of gas with foreign particles

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