Abstract
Wing-In-Ground (WIG) crafts has become one of the latest technologies in the marine vehicle sector. Improvements on WIG craft to increase aerodynamic performance has been done for decades. However, WIG crafts must be able to overcome significant hydrodynamic drag take-off from water surface and aerodynamic drag during flight. The current design of the hull-fuselage can cause flow separation and increase in drag hence flow control devices can be used to improve flow separation phenomenon on the hull-fuselage of the WIG craft. The objective of this study is to investigate the effect of flow control on the aerodynamics performance of WIG craft through wind tunnel experiments. From the results, CD values were reduced with the presence of flow control on WIG hull-fuselage. Different configurations on height, angle, and spacing of the flow control device helped in obtaining minimum CD. The flow control device was proven to reduce CD for up to 25% from the baseline model. This indicates that flow control device is helpful in improving aerodynamics performance of WIG craft.
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References
Tofa MM, Maimun A, Ahmed YM, Jamei S, Priyanto AR (2004) Experimental investigation of a wing-in-ground effect craft. Sci World J 2014
Qu Q, Lu Z, Liu P, Agarwal RK (2014) Numerical study of aerodynamics of a wing-in-ground-effect craft. J Aircraft 51(3):913–924
M X, Geisler R, Agocs J, Schroder A (2015) Investigation of coherent structures generated by acoustic tube in turbulent flow separation control. Exp Fluids 56(46)
Hudy LM, Naguib A (2007) Stochastic estimation of a separated-flow field using wall-pressure-array measurements. Phys Fluids 19:024103
Huerre P, Monkewitz PA (1985) Absolute and convective instabilities in free shear layers. J Fluid Mech 159:151–168
Wee D, Yi T, Annaswamy A, Ghoniem AF (2004) Self-sustained oscillation and vortex shedding in backward-facing step flow: simulation and linear instability analysis. Phys Fluids 16:3361–3373
Martin PB, Tung C, Hassan AA, Cerchie D, Roth J (2005) Active flow control measurements and CFD on a transport helicopter fuselage. In: Annual forum proceedings-American helicopter society, vol 61, no 1, American Helicopter Society, Inc.
Ben-Hamou E, Arad E, Seifert A (2007) Generic transport aft-body drag reduction using active flow control. Flow Turbul Combust 78(365)
Hazen DC (1967) Boundary layer control. J Fluid Mech 29:200–208
Saad MR, Zare-Behtash H, Che-Idris A, Konstatinos K (2012) Micro-ramps for hypersonic flow control. Micromachines 3(2):364–378
Sidhu BS, Saad MR, Ahmad KZK, Idris AC (2016) Riblets for airfoil drag reduction in subsonic flow. ARPN J Eng Appl Sci 11(12):7694–7698
Baljit SS, Saad MR, Nasib AZ, Sani A, Rahman MRA, Idris AC (2017) Suction and blowing flow control on airfoil for drag reduction in subsonic flow. J Phys Conf Ser 914(1):012009
Aliashak MZM, Saad MR, Latif AT, Idris AC, Rahman MRA (2018) Microvane in controlling noise in open cavity flow. IOP Conf Ser Mater Sci Eng 370(1):012016
Jumahadi MT, Saad MR, Idris AC, Sujipto S, Rahman MRA (2018) The potential of hybrid micro-vortex generators to control flow separation of NACA 4415 airfoil in subsonic flow. AIP Conf Proc 1930(1):020030
Godard G, Stanislas M (2006) Control of a decelerating boundary layer. Part 1 : optimization of passive vortex generators, vol 10, pp 181–191
Joslin RD, Miller DN (2009) Brief history of flow control. Brief history of flow control, pp 403–441
Vecchia PD, Nicolosi F (2014) Aerodynamic guidelines in the design and optimization of new regional turboprop aircraft. Aerosp Sci Technol 38:88–104
Kim BN, Chung MK (1995) Experimental study of roughness effects on the separated flow over a backward-facing step. AIAA J 33:159–161
Gardarin B, Jacquin L, Geffroy P (2008) Flow separation control with vortex generators, pp 1–17
Lin JC (2002) Review of research on low-profile vortex generators to control boundary-layer separation. Program Aerosp Sci 38:389–420
Acknowledgements
The authors would like to thank Mr. Muhammad Hafiz Bin Mahmood and the technical staffs of the Wind Tunnel Laboratory, Department of Mechanical Engineering, Faculty of Engineering, Universiti Pertahanan Nasional Malaysia (UPNM) for the technical assistance in using the equipment.
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Said, I., Abdul Rahman, M.R., Che Idris, A., Mohd Sakri, F., Saad, M.R. (2020). The Effect of Flow Control on Wing-In-Ground Craft Hull-Fuselage for Improved Aerodynamics Performance. In: Rajendran, P., Mazlan, N., Rahman, A., Suhadis, N., Razak, N., Abidin, M. (eds) Proceedings of International Conference of Aerospace and Mechanical Engineering 2019 . Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-15-4756-0_44
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DOI: https://doi.org/10.1007/978-981-15-4756-0_44
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