Supersonic flow past a system of two swept wedges mounted on a preliminary compression surface

DOI10.1134/S0015462813020130zbMath1269.76054OpenAlexW1967697086MaRDI QIDQ359313

Yu. P. Gun'ko, I. I. Mazhul'

Publication date: 9 August 2013

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

Full work available at URL: https://doi.org/10.1134/s0015462813020130

zbMATH Keywords

shocksinteraction between separation flowssupersonic velocitiesswept compression wedgesthree-dimensional boundary layer separation

Mathematics Subject Classification ID

Supersonic flows (76J20)

Related Items (1)

Numerical investigation of flow past a system of two sweptback compression wedges

Cites Work

• Supersonic inviscid corner flows with regular and irregular shock interaction
• Shock Wave-Boundary-Layer Interactions

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