Experimental investigation of the flow on a simple frigate shape (SFS)
- PMID: 24523646
- PMCID: PMC3913514
- DOI: 10.1155/2014/818132
Experimental investigation of the flow on a simple frigate shape (SFS)
Abstract
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.
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References
-
- Findlay DB, Ghee T. Experimental investigation of ship airwake flow control for a US Navy flight II-A class destroyer (DDG). Proceedings of the 3rd AIAA Flow Control Conference; June 2006; pp. 1303–1313. AIAA 2006-3501.
-
- Geyer WP, Long K, Carico D. Helicopter/Ship Qualification. Part 2: American Clearance Process. Vol. 22. RTO/NATO; 2003. RTO AG-300.
-
- Fang R, Booij PJA. NLR-TP-2006-024. National Aerospace Laboratory NLR; Helicopter-ship qualification testing. The Dutch clearance process.
-
- Bardera R. An experimental helicopter wind envelope for ship operations. World academy of science. Engineering and Technology. 2012;68:1362–1369.
-
- RTO Technical Report. TR-AVT-148. NATO; 2012. Modelling and simulation of the ship environment for safer aircraft launch and recovery. Final report of task group AVT-148.
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