For the interaction of shock waves with turbulent boundary layers, obtained experimental three-dimensional separation results and correlations with earlier two-dimensional and three-dimensional data are presented. It is shown that separation occurs much earlier for turbulent three-dimensional than for two-dimensional flow at hypersonic speeds.
Three-dimensional separation for interaction of shock waves with turbulent boundary layers
AIAA Journal ; 11
1973-11-01
Sonstige
Keine Angabe
Englisch
Analysis of transonic shock interaction with nonadiabatic turbulent boundary layers
Tema Archiv | 1976
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