Calculation of supersonic flow past wings with consideration of tangential discontinuities shed from the edges within the scope of a model using a system of Euler equations

DOI10.1007/BF01094460zbMath0449.76040MaRDI QIDQ1147591

A. N. Minajlos

Publication date: 1978

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

zbMATH Keywords

stationarytangential discontinuityslender wing

Mathematics Subject Classification ID

Supersonic flows (76J20) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Numerical methods for partial differential equations, boundary value problems (65N99)

Related Items (1)

Processing of gasdynamic numerical solutions in similarity parameters

Cites Work

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