WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEEDS OF A SPOILER-SLOT- DEFLECTOR COMBINATION ON A NACA 65A006 WING WITH QUARTER-CHORD LINE SWEPT BACK 32.6
This technical study examines a spoiler-slot-deflector combination mounted on a NACA 65A006 wing with a 32.6-degree quarter-chord sweep. Centered on wind-tunnel investigation at high subsonic speeds, it offers focused material for readers interested in aerodynamic configurations, experimental methods, and aerospace engineering.
About This Book
This technical work presents a wind-tunnel investigation conducted at high subsonic speeds.
It focuses on a spoiler-slot-deflector combination applied to a NACA 65A006 wing.
The wing configuration includes a quarter-chord line swept back 32.6 degrees.
The subject will interest readers studying aerodynamic testing, wing configurations, and high-speed airflow behavior.
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