Experimental and numerical analysis of the structure of pseudo-shock systems in Laval nozzles with parallel side walls

DOI10.1007/s00193-010-0263-1zbMath1262.76051OpenAlexW2024133014MaRDI QIDQ633507

T. Gawehn, A. Gülhan, N. S. Al-Hasan, Günter H. Schnerr

Publication date: 1 April 2011

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

Full work available at URL: https://doi.org/10.1007/s00193-010-0263-1

zbMATH Keywords

secondary flowCFDshock boundary layer interactiondouble chokedlaval nozzlepseudo-shock systemshock train

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05)

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Assessment of turbulence modeling for gas flow in two-dimensional convergent-divergent rocket nozzle ⋮ On the origin and propagation of perturbations that cause shock train inherent unsteadiness

Cites Work

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• Shock and wave dynamics in cavitating compressible liquid flows in injection nozzles
• Nozzle flow separation
• Shock structure in separated nozzle flows
• Shock wave boundary layer interaction
• Some physical aspects of shock wave/boundary layer interactions
• Type III and type IV shock/shock interferences: theoretical and experimental aspects
• An explicit algebraic Reynolds stress model for incompressible and compressible turbulent flows

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