Numerical modeling of supersonic flow over wings with varying aspect ratio on a broad range of angles of attack using the law of plane sections

DOI10.1007/BF01052091zbMath0789.76059OpenAlexW2040565198MaRDI QIDQ1317696

I. M. Panteleev, N. V. Voevodenko

Publication date: 12 April 1994

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01052091

zbMATH Keywords

Godunov's methodSychev's theory

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Cites Work

• Hypersonic flow of gas over a slender wing of variable shape
• Three-dimensional hypersonic gas flow past slender bodies at high angles of attack
• Extension of hypersonic, high-incidence, slender-body similarity

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