Numerical solution of the problem of unsteady supersonic flow around the front part of the wings with a detached shock wave

DOI10.1016/0045-7825(79)90078-1zbMath0419.76036OpenAlexW2010545887MaRDI QIDQ1132711

G. P. Voskresenskij

Publication date: 1979

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(79)90078-1

zbMATH Keywords

Euler equationsnumerical solutioncurvilinear coordinate systemdetached shock wavedifference method of second orderfront part of wingsunsteady supersonic flow

Mathematics Subject Classification ID

Compressible fluids and gas dynamics (76N99) Supersonic flows (76J20) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Numerical solution of discretized equations for boundary value problems involving PDEs (65N22)

Related Items (2)

Numerical solution of the problem of unsteady supersonic flow around the front part of the wings with a detached shock wave ⋮ Computation of supersonic inviscid flow around wings with a detached shock wave

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