CFD Analysis of NACA 4412 Aerofoil Considering Ground Effect

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Suraj, S and Nivedha Sri, S S and Ragul Krishna, P and Jagatheaswaran, S and Manoj Kumar, P (2021) CFD Analysis of NACA 4412 Aerofoil Considering Ground Effect. In: Materials, Design, and Manufacturing for Sustainable Environment. Lecture Notes in Mechanical Engineering . Springer, Singapore, pp. 563-571. ISBN 9789811598098

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Official URL: https://doi.org/10.1007/978-981-15-9809-8_42

Abstract

The presence of ground can affect the lift and drag forces during the take-off and landing of an aircraft. A two-dimensional, steady-state, turbulent CFD model for flow over a NACA4412 aerofoil is developed for studying the ground effect on the aerofoil. The Spalart–Allmaras model was used to solve for the turbulent flow. The scope of the study is limited for three different angle of attack (0°, 5° and 10°) and for the h/c ratios of 0.5, 1.0, and 2.0 and unbounded flow.

Item Type:	Book Section
Subjects:	F Mechanical Engineering > computational fluid dynamics
Divisions:	Mechanical Engineering
Depositing User:	Users 5 not found.
Date Deposited:	07 May 2024 10:40
Last Modified:	07 May 2024 10:40
URI:	https://ir.psgitech.ac.in/id/eprint/510

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