A new wall function method for hypersonic laminar boundary layers

DOI10.1017/JFM.2024.60OpenAlexW4391910792MaRDI QIDQ6200286

Unnamed Author, ZhenXun Gao

Publication date: 29 February 2024

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/jfm.2024.60

zbMATH Keywords

computational methodshypersonic flowcompressible boundary layers

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Cites Work

• Direct numerical simulation of hypersonic turbulent boundary layers. Part 4. Effect of high enthalpy
• Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature
• Near-wall model for compressible turbulent boundary layers based on an inverse velocity transformation

This page was built for publication: A new wall function method for hypersonic laminar boundary layers