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Numerical Simulation and Wind Tunnel Experiment on Pressure and Velocity Distribution Around the NACA0012 Airfoil for Optimising an Aerodynamic Model

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Advances in Fluid Mechanics and Solid Mechanics

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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.

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Correspondence to Motahar Reza .

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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

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  • DOI: https://doi.org/10.1007/978-981-15-0772-4_30

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  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-15-0771-7

  • Online ISBN: 978-981-15-0772-4

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