Derivation of higher approximations in the problem of special flows in plane Laval nozzles

DOI10.1016/0021-8928(78)90147-8zbMath0434.76055OpenAlexW1667152504MaRDI QIDQ1139995

A. L. Brezhnev, I. A. Chernov

Publication date: 1979

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(78)90147-8

zbMATH Keywords

special flowshigher approximationsoff-design modesplane Laval nozzlesself-similar componentsTaylor limit flow

Mathematics Subject Classification ID

Gas dynamics (general theory) (76N15) Supersonic flows (76J20)

Related Items (1)

On the asymptotic theory of sonic flow over bodies of revolution

Cites Work

• Plane transonic gas flows with singularities on the sonic line
• Algebraic self-modeling solutions of two-dimensional transonic gas flow
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