Abstract
The objective of the current study is to increase the lift and decrease the drag for NACA 0012 aerofoil by moving surface boundary-layer control (MSBC). The numerical simulation of lift and drag for two moving surfaces of aerofoil is carried out with commercial software “Ansys Fluent.” In the first configuration, one moving surface is considered of length 10% and other of length 15% of the chord length, both are at the upper side of the aerofoil. In the second configuration, both moving surfaces are considered of same length 10% of chord length but one is at the upper side, while other is at the lower side of the aerofoil. The results of both configurations are compared for different angle of attack and surface to free stream velocity ratio (Uc/U).
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Modi VJ, Ying B, Yokomizo T (1991) An approach to design of the next generation of fuel efficient trucks through aerodynamic drag reduction. In: Proceedings of the ASME winter annual meeting, Atlanta, USA, vol DE 40, pp 465–482
Modi VJ, Deshpande VS (2000) A Joukowski aerofoil with momentum injection. In: AIAA-2000-4108, pp 445–451
Schlichting H (1968) Boundary layer theory, 3rd edn. McGraw-Hill, New York, pp 127–724
Modi VJ, Munshi SR, Mokhtarian F, Bandyopadhyay G, Yokomizo T (1994) Multielement aerofoils with moving surface boundary-layer control: wind tunnel, numerical and flow visualization studies. In: Proceeding of the 19th congress of the International Council of the Aeronautics Sciences, Anaheim, USA. AIAA Publisher, pp 80–103
Modi VJ, Fernando M, Yokomizo T (1991) Moving surface boundary-layer control as applied to two-dimensional and three-dimensional bluff bodies. J Wind Eng Ind Aerodyn 38:83–92
Jawahar HK, Qing A, Mahdi A (2018) Experimental and numerical investigation of aerodynamic performance for aerofoils with morphed trailing edges. Renew Energy 127:355–367
Douvi C, Athanasios TI, Dionissios MP (2012) Evaluation of the turbulence models for the simulation of the flow over a National Advisory Committee for Aeronautics (NACA) 0012 aerofoil. J Mech Eng Res 4(3):100–111
Rao TS, Mahapatra T, Chaitanya S (2018) Enhancement of lift-drag characteristics of NACA 0012. Mater Today: Proc 5:5328–5337
Sahu R, Patnaik BSV (2011) CFD simulation of momentum injection control past a streamlined body. Int J Numer Meth Heat Fluid Flow 21(8):980–1001
Md. Sadiqul I, Shaik MH, Mohammad A, Md. Quamrul I (2017) Numerical investigation on boundary layer control through moving surface in NACA 0012 aerofoil. In: AIP conference proceedings, vol 1851, 020111, pp 1–7
Shmilovich A, Yadlin Y (2006) Flow control for the systematic build-up of high-lift systems. In: 3rd AIAA flow control conference, vol 2855, pp 1–14
Salam A, Barman S, Atique A, Asif S, Probha NN, Faisal Kh (2015) A CFD based parametric study to investigate the moving surface effect on aerofoil boundary-layer control. Military Institute of Science and Technology, Dhaka
Modi VJ, Mokhtarian F, Fernando M (1989) Moving surface boundary-layer control as applied to two-dimensional aerofoils. J Aircr 28(2):104–112
Hassan A, Sankar LN (1989) Separation control using moving surface effects—A numerical solution. AIAA 89(0972):1–9
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2020 Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Patel, V., Parekh, S., Parwani, A.K. (2020). Numerical Simulation of Moving Surface Boundary-Layer Control Over Symmetric Aerofoil. In: Parwani, A., Ramkumar, P. (eds) Recent Advances in Mechanical Infrastructure. Lecture Notes in Intelligent Transportation and Infrastructure. Springer, Singapore. https://doi.org/10.1007/978-981-32-9971-9_23
Download citation
DOI: https://doi.org/10.1007/978-981-32-9971-9_23
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-32-9970-2
Online ISBN: 978-981-32-9971-9
eBook Packages: EngineeringEngineering (R0)