 Calculated and Measured Pressure Distributions over the Midspan Section of the NACA 4412 Airfoil by Robert M. Pinkerton

ID: calculated-and-measured-pressure-distributions-over-the-midspan-section-of-the-naca-4412-airfoil-by-robert-m-pinkerton

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Calculated and Measured Pressure Distributions over the Midspan Section of the NACA 4412 Airfoil by Robert M. Pinkerton by

Codex  0 2026-11-05

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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