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2021 | OriginalPaper | Chapter

Multi-objective Optimization of Aerofoil

Authors : Prateet Dosi, Prem Kumar Bharti, Niharika Borah, Anjan Barman, Mriganka Baishnab, Soumyabrata Bhattacharjee

Published in: Advances in Industrial and Production Engineering

Publisher: Springer Singapore

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Abstract

NACA 0012 aerofoil has been optimized for maximum lift and minimum drag in different environmental conditions. This redevelopment has been achieved by two modern lift maximization techniques together, vortex generator and morphing. The vortex generator provides a proper path to the air flow that leads to increase in the lift, and morphing enables the structure of aerofoil to change according to the environmental conditions of flight. Keeping all the factors in mind, an aerofoil has been generated and optimized using ANSYS 14.0 software. The result indicates that the coefficient of lift (Cl) has increased in noticeable proportion of 16.67% and the coefficient of drag (Cd) has increased but in small proportion of 6.67%, which suggest that our target has been achieved.

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Title: Multi-objective Optimization of Aerofoil
Authors: Prateet Dosi
Prem Kumar Bharti
Niharika Borah
Anjan Barman
Mriganka Baishnab
Soumyabrata Bhattacharjee
Publisher: Springer Singapore
Book: Advances in Industrial and Production Engineering
Print ISBN: 978-981-334-319-1

Electronic ISBN: 978-981-334-320-7

Copyright Year: 2021
DOI: https://doi.org/10.1007/978-981-33-4320-7_71

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