On the study of transitional low-Reynolds number flows over airfoils operating at high angles of attack and their prediction using transitional turbulence models

J Wauters, J Degroote - Progress in Aerospace Sciences, 2018 - Elsevier
In this survey paper transitional turbulence modeling is approached from the point of view
relevant to small unmanned aerial vehicles (span≈ 1 m), of which the flow is characterized …

A study of long separation bubble on thick airfoils and its consequent effects

A Choudhry, M Arjomandi, R Kelso - International Journal of Heat and Fluid …, 2015 - Elsevier
A parametric study has been performed to analyse the flow around the thick-symmetric
NACA 0021 airfoil in order to better understand the characteristics and effects of long …

Performance of transition model for predicting low Re aerofoil flows without/with single and simultaneous blowing and suction

MS Genç, Ü Kaynak, H Yapici - European Journal of Mechanics-B/Fluids, 2011 - Elsevier
Transition-sensitive, single point eddy viscosity models are fairly new and performance
assessment of these models is required. In this study, the performance of transition and …

Numerical study of the effect of the Reynolds number and the turbulence intensity on the performance of the NACA 0018 airfoil at the low Reynolds number regime

J Michna, K Rogowski - Processes, 2022 - mdpi.com
In recent years, there has been an increased interest in the old NACA four-digit series when
designing wind turbines or small aircraft. One of the airfoils frequently used for this purpose …

A correlation-based algebraic transition model

SC Cakmakcioglu, O Bas… - Proceedings of the …, 2018 - journals.sagepub.com
A correlation-based algebraic transition model that relies on local flow information is
proposed. The model is qualified as an algebraic model, or a zero-equation model since it …

Engineering modeling of the laminar–turbulent transition: Achievements and problems

AV Boiko, SV Kirilovskiy, AA Maslov… - Journal of Applied …, 2015 - Springer
ENGINEERING MODELING OF THE LAMINAR–TURBULENT TRANSITION: ACHIEVEMENTS
AND PROBLEMS (REVIEW) UDC 532.526 AV Boiko, SV Ki Page 1 ISSN 0021-8944, Journal …

Flow over an aerofoil without and with a leading-edge slat at a transitional Reynolds number

MS Genç, Ü Kaynak, GD Lock - Proceedings of the …, 2009 - journals.sagepub.com
In this study, a multi-element aerofoil including NACA2415 aerofoil with NACA22 leading-
edge slat is experimentally and computationally investigated at a transitional Reynolds …

Mechanisms of surface pressure distribution within a laminar separation bubble at different Reynolds numbers

D Lee, S Kawai, T Nonomura, M Anyoji, H Aono… - Physics of …, 2015 - pubs.aip.org
Mechanisms behind the pressure distribution and skin friction within a laminar separation
bubble (LSB) are investigated by large-eddy simulations around a 5% thickness blunt flat …

Correlations for modeling transitional boundary layers under influences of freestream turbulence and pressure gradient

K Suluksna, P Dechaumphai, E Juntasaro - … Journal of Heat and Fluid Flow, 2009 - Elsevier
This paper presents mathematical expressions for two significant parameters which control
the onset location and length of transition in the γ–Reθ transition model of Menter et …

Low-reynolds-number aerodynamic performances of the NACA 0012 and Selig–Donovan 7003 Airfoils

JNN Counsil, K Goni Boulama - Journal of aircraft, 2013 - arc.aiaa.org
A comparative study of two airfoils at low Reynolds numbers using the transitional unsteady
Reynolds-averaged Navier–Stokes shear-stress transport γ-R e θ model and the ANSYS …