Direct computations of boundary layers distorted by migrating wakes in a linear compressor cascade

DOI10.1007/S10494-009-9216-0zbMath1423.76006OpenAlexW2123858383MaRDI QIDQ1037417

J. G. Wissink, Wolfgang Rodi, Paul A. Durbin, Tamer A. Zaki

Publication date: 16 November 2009

Published in: Flow, Turbulence and Combustion (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10494-009-9216-0

zbMATH Keywords

wakesseparationcompressorby-pass transition

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Software, source code, etc. for problems pertaining to fluid mechanics (76-04) Wakes and jets (76D25)

Related Items (5)

Large eddy simulation of a controlled diffusion compressor cascade ⋮ Transition induced by linear and nonlinear perturbation growth in flow past a compressor blade ⋮ Conditional sampling of transitional boundary layers in pressure gradients ⋮ Direct numerical simulations of transition in a compressor cascade: the influence of free-stream turbulence ⋮ Direct numerical simulation of heat transfer from the stagnation region of a heated cylinder affected by an impinging wake

Cites Work

• A numerical technique for two-dimensional grid generation with grid control at all of the boundaries
• Simulations of bypass transition
• Evidence of longitudinal vortices evolved from distorted wakes in a turbine passage
• BLADEROW INTERACTIONS, TRANSITION, AND HIGH-LIFT AEROFOILS IN LOW-PRESSURE TURBINES
• Direct numerical simulation of flow and heat transfer in a turbine cascade with incoming wakes
• Boundary-layer transition by interaction of discrete and continuous modes
• Simulation of boundary layer transition induced by periodically passing wakes
• Continuous mode transition and the effects of pressure gradient
• Mode interaction and the bypass route to transition

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