Open AccessTesting of a new algebraic laminar-turbulent transition model on a range of airfoils at moderate Reynolds numbers
Author(s) -
Alexey Matyushenko,
A. S. Stabnikov,
А. В. Гарбарук,
F. R. Menter,
Richard Lechner
Publication year - 2020
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1697/1/012229
Subject(s) - airfoil , reynolds averaged navier–stokes equations , laminar flow , turbulence , reynolds number , laminar turbulent transition , mechanics , algebraic number , range (aeronautics) , reynolds stress equation model , mathematics , statistical physics , computer science , physics , aerospace engineering , mathematical analysis , engineering , k epsilon turbulence model , k omega turbulence model
High quality prediction of laminar-turbulent transition for flow around airfoils is an important task for industrial applications. Prediction of such flows is usually carried out using the RANS framework in combination with transition models. The present study shows the capability of a recently developed algebraic transition model for prediction flows around different airfoils. The results of the model demonstrate satisfactory agreement with the experimental data and with results of existing differential models.