An efficient interacting boundary layer method for supersonic flow in the transonic regime

DOI10.1016/0045-7930(94)90026-4zbMath0784.76057OpenAlexW2045140810MaRDI QIDQ1309605

V. Pereyra

Publication date: 2 January 1994

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7930(94)90026-4

zbMATH Keywords

convergenceinviscid flowseparationalternating direction explicit accelerationlinear supersonic interaction lawnonlinear weak-shockparabolic humptransonic triple-deck solutions

Mathematics Subject Classification ID

Transonic flows (76H05) Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Cites Work

• Unnamed Item
• Shock-wave laminar boundary-layer interaction in supercritical transonic flow
• Laminar separation
• TRANSONIC LAMINAR BOUNDARY-LAYER FLOW NEAR CONVEX CORNERS
• New, quasi-simultaneous method to calculate interacting boundary layers
• Freely interacting transonic boundary layers
• Shock Wave Boundary-Layer Interactions in Laminar Transonic Flow
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate

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