Shock structure in separated nozzle flows

DOI10.1007/s00193-008-0173-7zbMath1255.76060OpenAlexW2037421992MaRDI QIDQ1932271

Marcello Onofri, Francesco Nasuti

Publication date: 17 January 2013

Published in: Shock Waves (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00193-008-0173-7

zbMATH Keywords

flow separationMach reflectionrocket nozzle

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20)

Related Items

Nozzle flow separation, Flow dynamics and wall-pressure signatures in a high-Reynolds-number overexpanded nozzle with free shock separation, Experimental and numerical analysis of the structure of pseudo-shock systems in Laval nozzles with parallel side walls

Cites Work

• On the impossibility of regular reflection of steady-state shock wave from the axis of symmetry
• A model to predict the Mach reflection of the separation shock in rocket nozzles