WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEEDS OF JET, SPOILER, AND AILERON CONTROLS ON A 1/16-SCALE MODEL OF THE DOUGLAS D-558-II RESEARCH AIRPLANE
Wind-tunnel tests at high subsonic speeds evaluate jet, spoiler, and aileron controls on a 1/16-scale model of the Douglas D-558-II research airplane.
About This Book
This report presents results from a wind-tunnel investigation conducted at high subsonic speeds.
The study examined jet, spoiler, and aileron controls on a 1/16-scale model of the Douglas D-558-II research airplane.
Data were collected to assess the aerodynamic performance of each control type under representative flight conditions.
The findings contribute to understanding control behavior for high-speed research aircraft design.
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