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Title: Airfoils for wind turbine

Patent ·
OSTI ID:873012

Airfoils for the tip and mid-span regions of a wind turbine blade have upper surface and lower surface shapes and contours between a leading edge and a trailing edge that minimize roughness effects of the airfoil and provide maximum lift coefficients that are largely insensitive to roughness effects. The airfoil in one embodiment is shaped and contoured to have a thickness in a range of about fourteen to seventeen percent, a Reynolds number in a range of about 1,500,000 to 2,000,000, and a maximum lift coefficient in a range of about 1.4 to 1.5. In another embodiment, the airfoil is shaped and contoured to have a thickness in a range of about fourteen percent to sixteen percent, a Reynolds number in a range of about 1,500,000 to 3,000,000, and a maximum lift coefficient in a range of about 0.7 to 1.5. Another embodiment of the airfoil is shaped and contoured to have a Reynolds in a range of about 1,500,000 to 4,000,000, and a maximum lift coefficient in a range of about 1.0 to 1.5.

Research Organization:
Midwest Research Institute, Kansas City, MO (United States)
DOE Contract Number:
AC36-83CH10093
Assignee:
Midwest Research Institute (Kansas City, MO)
Patent Number(s):
US 6068446
OSTI ID:
873012
Country of Publication:
United States
Language:
English

References (3)

Subsonic Natural-Laminar-Flow Airfoils book January 1992
Wing-section effects on the flight performance of a remotely pilotedvehicle journal October 1989
Thick airfoils for HAWTs journal January 1992