每年出版 6 期
ISSN 打印: 1948-2590
ISSN 在线: 1948-2604
ABOUT THE SECONDARY SEPARATION AT SUPERSONIC FLOW OVER A COMPRESSION RAMP
摘要
The numerical investigation of the separation at supersonic (M∞ = 5) flow over a compression ramp was carried out. The phenomenon of the secondary separation formation and development was considered in details. The separation stages were classified by a similarity parameter.
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Chiapparino Giuseppe, Stemmer Christian, Numerical investigation of a Mach 6 hypersonic laminar flow on two-dimensional cold-wall compression corners with controlled surface roughness, International Journal of Heat and Fluid Flow, 94, 2022. Crossref
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