Flow Characteristics Over a Lifting Wedge of Finite Aspect Ratio with Attached and Detached Chock Waves at a Mach Number of 1.40
This specialized study investigates flow characteristics over a lifting wedge of finite aspect ratio. It focuses on attached and detached chock waves under a Mach number of 1.40, offering a concise technical treatment for readers interested in aerodynamics, fluid mechanics, and engineering analysis.
About This Book
This technical work examines flow characteristics over a lifting wedge with finite aspect ratio.
The study focuses on attached and detached chock waves associated with the wedge configuration.
Its analysis is centered on conditions at a Mach number of 1.40.
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