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Birdwell, Carl (1955) Investigation at Low Speed of a Six-Percent Thick Symmetrical Circular-Arc Airfoil with Leading Edge Retraction in Combination with Nose Slot. Engineer's thesis, California Institute of Technology. doi:10.7907/B8SG-Y069. https://resolver.caltech.edu/CaltechETD:etd-12022003-154259

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