Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of spoiler-slot-deflector controls on thin untapered winds at transonic speeds / by Alex [Leather Bound]
Wind-tunnel investigation of spoiler-slot-deflector control effectiveness on thin untapered wings at transonic speeds, examining aspect ratio and chordwise location effects.
About This Book
This report presents findings from wind-tunnel tests on thin, untapered wings.
It investigates how aspect ratio and chordwise location affect spoiler-slot-deflector controls.
Tests were conducted at transonic speeds to evaluate aerodynamic performance.
The study provides data relevant to high-speed aircraft design considerations.
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