Computational study of unsteady turbulent flows around oscillating and ramping aerofoils

G.N. Barakos, D. Drikakis

Research output: Contribution to journalArticle

41 Citations (Scopus)

Abstract

The aim of this work is to computationally investigate subsonic and transonic turbulent flows around oscillating and ramping aerofoils under dynamic-stall conditions. The investigation is based on a high-resolution Godunov-type method and several turbulence closures. The Navier–Stokes and turbulence transport equations are solved in a strongly coupled fashion via an implicit-unfactored scheme. We present results from several computations of flows around oscillating and ramping aerofoils at various conditions in order to (i) assess the accuracy of different turbulence models and (ii) contribute towards a better understanding of dynamic-stall flows. The results show that the employed non-linear eddy-viscosity model generally improves the accuracy of the computations compared to linear models, but at low incidence angles the Spalart–Allmaras one-equation model was found to provide adequate results. Further, the computations reveal strong similarities between laminar and high-Reynolds number dynamic-stall flows as well as between ramping and oscillating aerofoil cases. Investigation of the Mach number effects on dynamic-stall reveals a delay of the stall angle within a range of Mach numbers. Investigation of the reduced frequency effects suggests the existence of an (almost) linear variation between pitch rate and stall angle, with higher slope at lower pitch rates. The pitch rate affects both the onset of dynamic-stall as well as the evolution of the associated vortical structures.
LanguageEnglish
Pages163-186
Number of pages24
JournalInternational Journal for Numerical Methods in Fluids
Volume42
Issue number2
DOIs
Publication statusPublished - 14 Apr 2003

Fingerprint

Unsteady Flow
Airfoils
Turbulent Flow
Turbulent flow
Angle
Mach number
Turbulence
Eddy Viscosity
Transonic Flow
Implicit Scheme
Turbulence Model
Turbulence models
Navier-Stokes
Transport Equation
Reynolds number
Linear Model
Incidence
Slope
Closure
High Resolution

Keywords

  • transonic turbulent flows
  • subsonic turbulent flows
  • oscillating aerofoils
  • ramping aerofoils
  • Godunov-type method
  • Navier–Stokes equations

Cite this

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abstract = "The aim of this work is to computationally investigate subsonic and transonic turbulent flows around oscillating and ramping aerofoils under dynamic-stall conditions. The investigation is based on a high-resolution Godunov-type method and several turbulence closures. The Navier–Stokes and turbulence transport equations are solved in a strongly coupled fashion via an implicit-unfactored scheme. We present results from several computations of flows around oscillating and ramping aerofoils at various conditions in order to (i) assess the accuracy of different turbulence models and (ii) contribute towards a better understanding of dynamic-stall flows. The results show that the employed non-linear eddy-viscosity model generally improves the accuracy of the computations compared to linear models, but at low incidence angles the Spalart–Allmaras one-equation model was found to provide adequate results. Further, the computations reveal strong similarities between laminar and high-Reynolds number dynamic-stall flows as well as between ramping and oscillating aerofoil cases. Investigation of the Mach number effects on dynamic-stall reveals a delay of the stall angle within a range of Mach numbers. Investigation of the reduced frequency effects suggests the existence of an (almost) linear variation between pitch rate and stall angle, with higher slope at lower pitch rates. The pitch rate affects both the onset of dynamic-stall as well as the evolution of the associated vortical structures.",
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Computational study of unsteady turbulent flows around oscillating and ramping aerofoils. / Barakos, G.N.; Drikakis, D.

In: International Journal for Numerical Methods in Fluids , Vol. 42, No. 2, 14.04.2003, p. 163-186.

Research output: Contribution to journalArticle

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