A model to predict the Mach reflection of the separation shock in rocket nozzles

DOI10.1007/978-3-540-85181-3_48zbMath1169.76373OpenAlexW2144626268MaRDI QIDQ3395810

Francesco Nasuti, Marcello Onofri

Publication date: 13 September 2009

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

Full work available at URL: https://doi.org/10.1007/978-3-540-85181-3_48

Mathematics Subject Classification ID

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

Related Items (2)

Nozzle flow separation ⋮ Shock structure in separated nozzle flows

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