p.3
p.9
p.15
p.21
p.29
p.37
p.45
p.51
p.63
Development of a Stall Barrier with Internal Flow Channel for Effective, Highly Separated Boundary Layer and Flow Control in the Rotor Blade Root Region
Abstract:
As part of a cluster project in the Aerospace research cluster at the Hochschule Bremen, the model rotor blade of a wind turbine is to be aerodynamically optimized with a more effective stall barrier. The flow element to be developed should provide very effective interruption of the radial flow on the rotor blade. A combination of this flow element and the "Splitflap" flow element allows the aerodynamic efficiency of the rotor blade to be further improved.
Info:
Periodical:
Pages:
29-35
Citation:
Online since:
December 2013
Keywords:
Price:
Сopyright:
© 2014 Trans Tech Publications Ltd. All Rights Reserved
Share:
Citation: