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...
| Main Authors: | , , , , |
|---|---|
| Format: | Conference or Workshop Item |
| Language: | English English |
| Published: |
2015
|
| Subjects: | |
| 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 |