Abstract
Airfoil design is a significant facet of aerodynamics. In this paper, optimise aerodynamic model for the NACA0012 airfoil shape has been studied based the wind tunnel experiment and numerical simulation using ANSYS. The velocity and pressure distribution around the NACA0012 airfoil has found by tests results which are compared with numerical simulation. Based on this experiment result, optimisations shape of the airfoil has been investigated.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Eleni DC (2012) Evaluation of the turbulence model for the simulation of the flow over a NACA 0012 airfoil. J Mech Eng Res 4(3):100–111
Ghose P, Dewangan AK, Mitra P, Rout AK (2012) Experimental study of aero foil with wind tunnel setup. In: Recent advances in thermal engineering (RATE-2014), OSC-366/ 2012
Shih TH, Liou WW, Shabbir A, Zhu J (1995) A new k-ε eddy-viscosity model for high reynold number turbulent flows. National Aeronautics and space Administration, USA, pp 1–32
Hossain S, Raiyan MD, Ferdous M (2014) A comparative flow analysis of NACA 6409 AND NACA 4412 aerofoil. Int J Res Eng Technol 03:342–350
Harris CD (1981) Two-dimensional aerodynamic characteristics of the NACA0012 airfoil in the Langley 8-foot transonic pressure tunnel. NASA-TM-81927
Goorjian PM, Guruswamy GP (1988) Transonic unsteady aerodynamic and aeroelastic calculations about airfoils and wings. Comput Struct 30(4):929–936
Wang SF, Wu Y (2003) Hierarchical evolutionary algorithms and its application in transonic airfoil optimization in aerodynamics. Chin J Aeronaut 16:1–6
Rumsey C (2018) 2DN00: 2D NACA 0012 airfoil validation case. https://turbmodels.larc.nasa.gov/naca0012_val.html
Ackeret J (1925) Luftkrafte auf Flugel, die mit der grosserer als Schallgeschwindigkeit bewegt werden. Zeitschrift fur Flugtechnik und Motorluftschiffahrt 16:72–74
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
Reza, M., Bhattacharyya, A.M., Sadangi, D.K., Kumar, A. (2020). Numerical Simulation and Wind Tunnel Experiment on Pressure and Velocity Distribution Around the NACA0012 Airfoil for Optimising an Aerodynamic Model. In: Maity, D., Siddheshwar, P., Saha, S. (eds) Advances in Fluid Mechanics and Solid Mechanics. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-15-0772-4_30
Download citation
DOI: https://doi.org/10.1007/978-981-15-0772-4_30
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-15-0771-7
Online ISBN: 978-981-15-0772-4
eBook Packages: EngineeringEngineering (R0)