Calculation of optimal surface roughness with respect to Lift/Drag forces acting on wind turbine blade

Xuerui Mao*, Simon Hogg

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Citations (Scopus)
Plum Print visual indicator of research metrics
  • Citations
    • Citation Indexes: 2
  • Captures
    • Readers: 3
see details

Abstract

Roughness on the surface of turbine blades induced by icing, dirt, erosion or manufacturing imperfections changes the aerodynamic configurations of wind turbines and reduces the power generation efficiency. In this work, a modified NACA0024 aerofoil is adopted to study effects of surface roughness on lift/drag forces. Three Reynolds numbers, 1000, 2000 and 5000 and a range of angles of attack [0°,20°] are studied. Since the magnitude of the roughness is small, it can be modelled as non-zero velocity boundary conditions imposed on the smooth surface without roughness. The flow with surface roughness can be therefore decomposed as the sum of a flow without roughness and a flow induced by roughness (or the velocity boundary conditions). The first flow can be obtained by solving the Navier-Stokes (NS) equation while the second one is governed by the linearized NS equation. Correspondingly the lift and drag forces acting on the aerofoil can be also decomposed as the sum of a force without considering roughness and a force induced by roughness. Instead of studying a particular type or distribution of roughness, we calculate the optimal roughness, which changes aerodynamic forces most effectively. This optimal roughness is obtained through a sensitivity study by solving an adjoint equation of the linearized NS equation. It is found that the optimal roughness with respect to both drag and lift forces is concentrated around the trailing edge and upper leading edge of the aerofoil and the lift is much more sensitive to roughness than the drag. Then the optimal roughness with a small magnitude is added to the smooth aerofoil geometry and this new geometry is tested through direct numerical simulations (DNS). It is found that the optimal roughness with a small magnitude (e-norm, defined as the square integration of the roughness around the surface, 0.001) induces over 10% change of the lift. Comparing the forces acting on the smooth surface and on the rough surface, it is noticed that the roughness changes the pressure force significantly while has little influence on the viscous forces. The pressure distribution is further inspected to study mechanisms of the effects of roughness on forces.

Original languageEnglish
Title of host publicationASME Turbo Expo 2014
Subtitle of host publicationTurbine Technical Conference and Exposition, GT 2014
PublisherAmerican Society of Mechanical Engineers (ASME)
ISBN (Electronic)9780791845660
DOIs
Publication statusPublished - 2014
Externally publishedYes
EventASME Turbo Expo 2014: Turbine Technical Conference and Exposition, GT 2014 - Dusseldorf, Germany
Duration: 16 Jun 201420 Jun 2014

Publication series

NameProceedings of the ASME Turbo Expo
Volume3B

Conference

ConferenceASME Turbo Expo 2014: Turbine Technical Conference and Exposition, GT 2014
Country/TerritoryGermany
CityDusseldorf
Period16/06/1420/06/14

Fingerprint

Dive into the research topics of 'Calculation of optimal surface roughness with respect to Lift/Drag forces acting on wind turbine blade'. Together they form a unique fingerprint.

Cite this

Mao, X., & Hogg, S. (2014). Calculation of optimal surface roughness with respect to Lift/Drag forces acting on wind turbine blade. In ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, GT 2014 (Proceedings of the ASME Turbo Expo; Vol. 3B). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/GT2014-25416