Two-dimensional low-Reynolds number wind tunnel results for airfoil NACA 0018

Wind Engineering

Volumn 32, Issue 6, 2008, Pages 525-537

  Timmer, W A ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLES OF ATTACK; LAMINAR SEPARATION BUBBLE; LAMINAR SEPARATIONS; LOW REYNOLDS NUMBER; MOMENT CURVE; NOISE REDUCTIONS; PERFORMANCE CALCULATION; RADIATED NOISE; THREE-DIMENSIONAL PATTERNS; VERTICAL AXIS WIND TURBINES;

ACOUSTIC NOISE MEASUREMENT; AIRFOILS; HYSTERESIS; HYSTERESIS LOOPS; LAMINAR FLOW; REYNOLDS NUMBER; WIND POWER; WIND TURBINES;

TWO DIMENSIONAL;

AIR BUBBLE; DRAG COEFFICIENT; PERFORMANCE ASSESSMENT; REYNOLDS NUMBER; TWO-DIMENSIONAL MODELING; WIND TUNNEL; WIND TURBINE;

EID: 67650082543     PISSN: 0309524X     EISSN: None     Source Type: Journal    
DOI: 10.1260/030952408787548848     Document Type: Article

References (6)

1. Website of the Turby vertical axis turbine, www.turby.nl
2. R. van Rooij, "Modification of the boundary layer calculation in RFOIL for improved airfoil stall prediction". Report IW-96087R, TU-Delft, the Netherlands
3. H.C. Garner, E.W.E. Rogers, W.E.A. Acum and E.C. Maskell, "Subsonic wind tunnel wall corrections". AGARDograph 109, October 1966
4. B.F.R. Ewald (Ed.), "Wind tunnel wall corrections". AGARDograph 336, October 1998
5. T. Nakano et al. "Experimental study on flow and noise characteristics of NACA 0018 airfoil". Journal of Wind Engineering and Industrial Aerodynamics 95 (2007) pp 511-531
6. Jacobs, Eastman N Sherman, Albert. "Airfoil section characteristics as affected by variations of the Reynolds number". NACA Report 586, (1937).