| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 4917897 | Composite Structures | 2017 | 13 Pages |
Abstract
An improved distribution of both chord values and twist angles is determined, as well as an optimal layout of the blade composite skin. A slight increase in the aerodynamic power generation is obtained, as well as a marked improvement in overall blade deformation characteristics.
Related Topics
Physical Sciences and Engineering
Engineering
Civil and Structural Engineering
Authors
Andrea Dal Monte, Stefano De Betta, Marco Raciti Castelli, Ernesto Benini,