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 Tagged: Work by Robert M. Pinkerton

Calculated and Measured Pressure Distributions over the Midspan Section of the NACA 4412 Airfoil by Robert M. Pinkerton 2026-11-05
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ntrs.nasa.gov/citations/19930091638
NACA-TR-563 (1937). NTRS abstract: 54 pressure orifices, a 5-by-30-inch model, 17 angles from −20 to 30 degrees, Reynolds number approximately 3 million; comparison with potential-flow calculations.
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The Characteristics of 78 Related Airfoil Sections from Tests in the Variable-Density Wind Tunnel by Eastman N. Jacobs and others 2026-11-05
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ntrs.nasa.gov/citations/19930091108
NACA Report 460, originally published November 1933; primary PDF: ntrs.nasa.gov/api/citations/19930091108/downloads/19930091108.pdf . Apparatus and Methods describes duralumin models, dimensions, Reynolds number, tank pressure and measured forces/moments. The introduction and profile derivation explain systematic variation of thickness and mean-line form.
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Total articles: 2
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