Abstract
Experiments on a large-scale Flettner rotor were carried out in the boundary-layer test section of Politecnico di Milano wind tunnel. The rotating cylinder used in the experimental campaign (referred to as Delft Rotor) had a diameter of 1.0 m and span of 3.73 m. The Delft Rotor was equipped with two purpose-built force balances and two different systems to measure the pressure on the rotor’s outer skin. The goal of the experiments was to study the influence of different Reynolds numbers on the aerodynamic forces generated by the spinning cylinder. The highest Reynolds number achieved during the experiments was \( {\text{Re}} = 1.0 \cdot 10^{6} \).
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References
Badalamenti C, Prince SA (2008) The effects of endplates on a rotating cylinder in crossflow. In: 26th AIAA applied aerodynamics conference, Honolulu, HI, USA, 18–21 August
Bergeson L, Greenwald CK (1985) Sail assist developments 1979–1985. J Wind Eng Ind Aerodyn 19:45–114
Clayton BR (1985) BWEA initiative on wind assisted ship propulsion (WASP). J Wind Eng Ind Aerodyn 19:251–276
Craft TJ, Iacovides H, Johnson N, Launder BE (2012) Back to the future: Flettner-Thom rotors for maritime propulsion? In: 7th international symposium on turbulence heat and mass transfer, Palermo, Italy, 24–27 September
Everts M, Ebrahim R, Kruger JP, Miles E, Sharifpur M, Meyer JP (2014) Turbulent flow across a rotating cylinder with surface roughness. In: 10th international conference on heat transfer, fluid mechanics and thermodynamics, Orlando, FL, USA, 14–16 July
Kayser LD, Clay WH, Damico Jr WP (1986) Surface pressure measurements on a 155 mm projectile in free-flight at transonic speed. In: 14th aerodynamic testing conference, West Palm Beach, FL, USA, 5–7 March
Kurtz AD, Ainsworth RW, Thorpe SJ, Ned A (2003) Further work on acceleration insensitive semiconductor pressure sensor for high bandwidth measurements on rotating turbine blades. In: NASA propulsion measurement sensor development workshop, Huntsville, AL, USA, 13–15 May
Lafay A (1912) Contribution Experimentale a l’Aerodynamique du Cylindre. Reveus Mechanique 30:417–442
McLaughlin TE, Stephen EJ, Robinson MC (1991) Pressure measurements on a rotating circular cylinder. AIAA-91-3265-CP
Miller MC (1976) Surface pressure measurements on a spinning wind tunnel model. AIAA J 14:1669–1670
Pollack FG, Liebert CH, Peterson VS (1972) Rotating pressure measuring system for turbine cooling investigations. Technical report TM X-2621, NASA
Reid EG (1924) Tests of rotating cylinders. Technical report TN-209, NACA
Rollstin LR (1990) Measurement of in-flight base pressure on an artillery-fired projectile. J Spacecraft Rockets 27:5–6
Swanson WM (1961) The Magnus effect: a summary of investigations to date. J Basic Eng 83:461–470
Thom A (1926) The aerodynamics of a rotating cylinder. PhD thesis, University of Glasgow, UK
Thom A (1931) Experiments on the flow past a rotating cylinder. Technical report R&M No. 1410, Aeronautical Research Council
Thom A, Sengupta SR (1932) Air torque on a cylinder rotating in an air stream. Technical report R&M No. 1520, Aeronautical Research Council
Thom A (1934) Effects of discs on the air forces on a rotating cylinder. Technical report R&M No. 1623, Aeronautical Research Council
Zdravkovich MM (2003) Flow around circular cylinders, volume 2: applications. Oxford University Press Inc., New York
Acknowledgements
This research was supported by the Sea Axe Fund. The author would like to thank the research sponsor as well as all the staff at Politecnico di Milano wind tunnel for their kind help.
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Bordogna, G. et al. (2019). Wind-Tunnel Experiments on a Large-Scale Flettner Rotor. In: Ricciardelli, F., Avossa, A. (eds) Proceedings of the XV Conference of the Italian Association for Wind Engineering. IN VENTO 2018. Lecture Notes in Civil Engineering, vol 27. Springer, Cham. https://doi.org/10.1007/978-3-030-12815-9_9
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