The influence of free-stream turbulence intensity on the performance of Gurney-flap equipped wind-turbine blades
Conference
·
OSTI ID:372130
- Univ. of Calgary, Alberta (Canada). Dept. of Mechanical Engineering
A study is presented of apparent drag anomalies based on the results of measurements made by many workers. In some cases the addition, to an airfoil, of a Gurney flap adds little or nothing to the airfoil drag coefficient; yet in other cases, for a prescribed Gurney-flap height-to-chord ratio, the addition of the Gurney flap can increase the airfoil drag coefficient,m at low lift coefficients, by a factor as large as three. The lift increment obtained is essentially independent of the drag level recorded and is, to a first approximation, proportional to the height-to-chord ratio of the Gurney flap. It is, as a consequence of the study, shown that the major adverse influence on the drag coefficient of Gurney-flap equipped airfoils is the thinness of the pressure-surface boundary layer at the airfoil trailing edge. It has been shown by other workers that provided the height of a Gurney flap is less than the boundary layer thickness, the drag penalty due to the Gurney flap is small or can be essentially zero. The influence of the chord-based Reynolds number on the pressure-surface boundary layer thickness appears to parallel that associated with a turbulent flow over a flat plate. Hence the boundary layer thickness diminishes with increasing chord-based Reynolds number. A factor that is shown to have a major impact on the boundary layer thickness is the inherent turbulence level of the approaching flow. Generally, the higher the turbulence level and the lower the Reynolds number, the thicker, for a prescribed airfoil chord, the boundary layer.
- OSTI ID:
- 372130
- Report Number(s):
- CONF-960154--; ISBN 0-9648731-8-4
- Country of Publication:
- United States
- Language:
- English
Similar Records
Effect of Blade Roughness on Transition and Wind Turbine Performance.
Effect of Flap Deflection on Section Characteristics of S813 Airfoil; Period of Performance: 1993--1994
Post stall airfoil data for wind turbines: wind tunnel test results
Program Document
·
Tue Sep 01 00:00:00 EDT 2015
·
OSTI ID:1427238
Effect of Flap Deflection on Section Characteristics of S813 Airfoil; Period of Performance: 1993--1994
Technical Report
·
Fri Dec 31 23:00:00 EST 2004
·
OSTI ID:15011677
Post stall airfoil data for wind turbines: wind tunnel test results
Technical Report
·
Sun Jul 01 00:00:00 EDT 1984
·
OSTI ID:6165655