Delayed detached eddy simulation of the end-effect regime and side-loads in an overexpanded nozzle flow

DOI10.1007/s00193-009-0199-5zbMath1255.76041OpenAlexW1981488342MaRDI QIDQ1932272

Sébastien Deck

Publication date: 17 January 2013

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

Full work available at URL: https://doi.org/10.1007/s00193-009-0199-5

zbMATH Keywords

separated flownozzleunsteadydelayed detached eddy simulationrestricted-shock-separationside-loads

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite volume methods applied to problems in fluid mechanics (76M12) Supersonic flows (76J20)

Related Items (5)

Nozzle flow separation ⋮ Flow dynamics and wall-pressure signatures in a high-Reynolds-number overexpanded nozzle with free shock separation ⋮ Unsteadiness in shock-induced separated flow with subsequent reattachment of supersonic annular jet ⋮ Compressibility effects on the vortical flow over a 65° sweep delta wing ⋮ Jet resonance in truncated ideally contoured nozzles

Cites Work

• Unsteadiness of flow separation and end-effects regime in a thrust-optimized contour rocket nozzle
• A new version of detached-eddy simulation, resistant to ambiguous grid densities
• On coherent-vortex identification in turbulence
• Development and application of Spalart–Allmaras one equation turbulence model to three-dimensional supersonic complex configurations
• On the identification of a vortex
• Multiscale and Multiresolution Approaches in Turbulence
• Unsteadiness of an axisymmetric separating-reattaching flow: Numerical investigation
• Numerical investigation of transitional supersonic axisymmetric wakes
• Numerical simulation of the compressible mixing layer past an axisymmetric trailing edge

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