An inverse design method for cascades for low-Reynolds number flow

DOI10.5402/2012/148607zbMath1264.76093OpenAlexW2041760048WikidataQ58689878 ScholiaQ58689878MaRDI QIDQ1954342

Martin Böhle

Publication date: 11 June 2013

Published in: ISRN Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.5402/2012/148607

zbMATH Keywords

low Reynolds numberturbulent boundary layer flow

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Direct numerical and large eddy simulation of turbulence (76F65) Hydro- and aero-acoustics (76Q05) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Uses Software

• Spalart-Allmaras

Cites Work

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• Some properties of boundary layer flow during the transition from laminar to turbulent motion
• The prediction of separation of the turbulent boundary layer
• A compressible three-dimensional design method for radial and mixed flow turbomachinery blades
• Viscous-inviscid analysis of transonic and low Reynolds number airfoils

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