A 16%-thick, natural-laminar-flow airfoil, the S829, for the tip region of 20- to 40-meter-diameter, stall-regulated, horizontal-axis wind turbines has been designed and analyzed theoretically. The two primary objectives of restrained maximum lift, insensitive to roughness, and low profile drag have been achieved. The constraints on the pitching moment and the airfoil thickness have been satisfied. The airfoil should exhibit a docile stall.
S829 Airfoil. Period of Performance: 1994-1995
2005
40 pages
Report
No indication
English
Online Contents | 1994
Konstruktions-Jahrbuch 1994/1995
IuD Bahn | 1994
|Veröffentlichungszeitraum Januar 1994-Juni 1995
Online Contents | 1995
The 1994-1995 Antarctic Field Season
SAE Technical Papers | 1995
|Jahrbuch der Schweizerischen Verkehrswirtschaft 1994/1995
IuD Bahn | 1995
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