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2020 | OriginalPaper | Chapter

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

Authors : Motahar Reza, Anindita M. Bhattacharyya, Deepak K. Sadangi, Aman Kumar

Published in: Advances in Fluid Mechanics and Solid Mechanics

Publisher: Springer Singapore

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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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previous chapter Probability of Failure of a Beam Subjected to Randomly Moving Loads
Literature
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Metadata
Title
Numerical Simulation and Wind Tunnel Experiment on Pressure and Velocity Distribution Around the NACA0012 Airfoil for Optimising an Aerodynamic Model
Authors
Motahar Reza
Anindita M. Bhattacharyya
Deepak K. Sadangi
Aman Kumar
Copyright Year
2020
Publisher
Springer Singapore
Book
Advances in Fluid Mechanics and Solid Mechanics

Print ISBN: 978-981-15-0771-7

Electronic ISBN: 978-981-15-0772-4

Copyright Year: 2020

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

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