This work explores spanwise loading as a primary aerodynamic design variable, using an oblique flying wing to study how twist distribution and slew angle reshape performance and stability. Instead of starting from the assumption that a wing’s planform alone determines its behavior, the research examines how deliberately redistributing lift along the span can change rolling, pitching, and yawing tendencies as well as the character of the wake. The result is a more design-centered view of spanloading, where aerodynamic efficiency and stability are treated as consequences of how lift is arranged across the wing rather than how much lift is produced overall.
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Power of Geometric Wing Twist
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Effects Of Spanloading And Slew Angle On An Oblique Flying Wing
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Effects Of Spanloading And Slew Angle On An Oblique Flying Wing. 2020.