Effect of Thickness, Camber, and Thickness Distribution on Airfoil Characteristics at Mach Numbers up to 1.0
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Daley, Bernard N↗
Engineering topics
Dick, Richard S
Publications and source records attributed to Dick, Richard S.
Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0
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Daley, Bernard N↗
Two-dimensional Chord-wise Load Distributions at Transonic Speeds
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Lindsey, Walter F↗