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The Scientific World Journal
Volume 2014 (2014), Article ID 818132, 8 pages
Research Article

Experimental Investigation of the Flow on a Simple Frigate Shape (SFS)

INTA, Experimental Aerodynamics Branch, carretera de Ajalvir p. k. 4.5, 28850 Madrid, Spain

Received 30 August 2013; Accepted 8 October 2013; Published 12 January 2014

Academic Editors: P.-C. Chen and M. G. Perhinschi

Copyright © 2014 Rafael Bardera Mora. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.


Helicopters operations on board ships require special procedures introducing additional limitations known as ship helicopter operational limitations (SHOLs) which are a priority for all navies. This paper presents the main results obtained from the experimental investigation of a simple frigate shape (SFS) which is a typical case of study in experimental and computational aerodynamics. The results obtained in this investigation are used to make an assessment of the flow predicted by the SFS geometry in comparison with experimental data obtained testing a ship model (reduced scale) in the wind tunnel and on board (full scale) measurements performed on a real frigate type ship geometry.