IIUM Repository (IREP)

Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device

Asrar, Waqar and Altaf, Afaq and Omar, Ashraf Ali and Hrairi, Meftah and Thong , Boon Tan (2015) Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device. In: 8th Ankara International Aerospace Conference, 10-12 Sep 2015, Ankara, Turkey.

[img] PDF - Published Version
Restricted to Registered users only

Download (406kB) | Request a copy
[img] PDF
Download (783kB)

Abstract

A six component force balance was used to obtain the aerodynamic performance of a NACA 23012 half wing model with a slender reverse delta type add-on device in landing configuration (slat deflection 15° and flap deflection 20°) at a chord-based Reynolds number of Rec =2.74×105. Reverse delta type add-on devices of three different sizes were tested. It was found that the aerodynamic performance of the half wing model was only slightly affected by the use of a reverse delta type addon device. It was found that the reduction in lift is 4.9% and the increase in drag is 15.2%.

Item Type: Conference or Workshop Item (Plenary Papers)
Additional Information: 4277/46153 ISBN 978-605-65900-1-6
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL500 Aeronautics
Kulliyyahs/Centres/Divisions/Institutes: Kulliyyah of Engineering
Kulliyyah of Engineering > Department of Mechanical Engineering
Depositing User: Prof. Waqar Asrar
Date Deposited: 27 Jan 2016 08:25
Last Modified: 18 Jul 2016 17:05
URI: http://irep.iium.edu.my/id/eprint/46153

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year