Research Output | Dar Al-hikmah Library | IIUM Only
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 test