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Scale analysis and experimental observations of shock-induced turbulent boundary layer separation in nozzles

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Publication:885959
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DOI10.1016/j.euromechflu.2006.10.002zbMath1111.76304OpenAlexW2144710900MaRDI QIDQ885959

Russell G. Keanini, Andrew M. Brown

Publication date: 14 June 2007

Published in: European Journal of Mechanics. B. Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.euromechflu.2006.10.002


zbMATH Keywords

supersonic flowoverexpanded nozzle flow


Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) Shock waves and blast waves in fluid mechanics (76L05) Turbulent boundary layers (76F40) Compressibility effects in turbulence (76F50)


Related Items (2)

Momentum balance based model for predicting the scale of separation bubbles induced by incident shock wave/turbulent boundary layer interactions ⋮ Stochastic rocket dynamics under random nozzle side loads: Ornstein-Uhlenbeck boundary layer separation and its coarse grained connection to side loading and rocket response




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