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

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

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...

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Bibliographic Details
Main Authors:	Asrar, Waqar, Altaf, Afaq, Omar, Ashraf Ali, Hrairi, Meftah, Thong , Boon Tan
Format:	Proceeding Paper
Language:	English English
Published:	2015
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/46153/ http://irep.iium.edu.my/46153/1/AIAC-2015-040.pdf http://irep.iium.edu.my/46153/4/AIAC_2015_Ankara_conference.docx

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