Preliminary Investigation of Spoiler Lateral Control on a 42 deg Sweptback Wing at Transonic Speeds
by Schneiter, Leslie E. ; Ziff, Howard L.
A specialized aerospace engineering study examining spoiler lateral control on a 42-degree sweptback wing at transonic speeds. Written by Leslie E. Schneiter and Howard L. Ziff, this work addresses aerodynamic control behavior in a high-speed flight context.
About This Book
This technical work examines spoiler lateral control on a wing swept back 42 degrees.
The investigation focuses on aerodynamic behavior at transonic speeds.
It presents a specialized study relevant to aircraft design, wing control, and high-speed aeronautics.
The authors are Leslie E. Schneiter and Howard L. Ziff.
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