| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 5472972 | Aerospace Science and Technology | 2017 | 20 Pages |
Abstract
A special challenge of this research was to overcome scaling between available the wind tunnel missile model geometry, used for aerodynamic experiments, and the real fin geometry model, used for static structural experiments.
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Nenad VidanoviÄ, BoÅ¡ko RaÅ¡uo, Gordana KastratoviÄ, Stevan MaksimoviÄ, DuÅ¡an ÄurÄiÄ, Marija SamardžiÄ,