Experimental investigation of flow past simple model bodies in hypersonic wind tunnels at similar values of the Mach and Reynolds numbers but at different physical flow velocities

DOI10.1134/S0015462815010123zbMath1325.76006OpenAlexW2020931187MaRDI QIDQ893521

V. I. Alferov, A. S. Bushmin, I. V. Egorov

Publication date: 19 November 2015

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

Full work available at URL: https://doi.org/10.1134/s0015462815010123

zbMATH Keywords

visualizationconepressure distributioncalculation methodsbow shock stand-off distancehypersonic gas flowsmodels bodies (hemispherewedge)wind tunnels

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Hypersonic flows (76K05)

Cites Work

• Accurate Numerical Methods for Boundary-Layer Flows. II: Two Dimensional Turbulent Flows
• Unnamed Item
• Unnamed Item

This page was built for publication: Experimental investigation of flow past simple model bodies in hypersonic wind tunnels at similar values of the Mach and Reynolds numbers but at different physical flow velocities