Low speed aerodynamic performance experimental study of NACA 23012 half-span wing

Altaf, Afaq and Aldheeb, Mohammed and Omar, Ashraf Ali and Asrar, Waqar (2026) Low speed aerodynamic performance experimental study of NACA 23012 half-span wing. Journal of Aerospace Technology and Management, 18 (e3326). pp. 1-10. ISSN 2175-9146

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Abstract

A six-component force balance was used to obtain the aerodynamic performance of a NACA 23012 half-span wing model at low freestream speeds of 20 m·s-1 to 50 m·s-1. The half-span wing model is equipped with a leading-edge slat and a trailing-edge flap. The impact on aerodynamic performance by the slat and flap configurations of the half-span wing model is studied. Abundant high Reynolds number aerodynamic performance studies have been carried out on various well-known airfoil profiles, but low-speed aerodynamic performance studies are limited. This work will be used as a benchmark study to support researchers working on NACA 23012 airfoils or wings at low speeds.

Item Type:	Article (Journal)
Uncontrolled Keywords:	NACA 23012; Aerodynamic performance; Slat; Flap; High lift configuration
Subjects:	T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL500 Aeronautics
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button):	Kulliyyah of Engineering > Department of Mechanical Engineering
Depositing User:	Dr Mohammed Aldheeb
Date Deposited:	30 Sep 2026 09:18
Last Update:	30 Sep 2026 09:18
Queue Number:	2026-09-Q5329
URI:	http://irep.iium.edu.my/id/eprint/131586
Indexed In:	WOS and SCOPUS, Google Scholar

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