Navier-Stokes Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code - A Sensitivity Study

DOI10.1007/978-3-540-33287-9_24zbMath1323.76056OpenAlexW1515798009MaRDI QIDQ3196464

Andreas Krumbein

Publication date: 29 October 2015

Published in: New Results in Numerical and Experimental Fluid Mechanics V (Search for Journal in Brave)

Full work available at URL: https://elib.dlr.de/19538/1/STAB_2004.Krumbein.Manuscript_CORRECTIONS.after.Review_with_highQUALITY-Pix.pdf

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (3)

Reynolds Stress Turbulence Modelling with γ Transition Model ⋮ Transition prediction for three-dimensional flows using parallel computation ⋮ Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction Using the DLR TAU Code

Uses Software

• MEGAFLOW

Cites Work

• Unnamed Item

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