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Turbulent boundary layer wall pressure flight data

Published by Albert Allen | National Aeronautics and Space Administration | Catalog Last Checked: February 14, 2026 at 08:24 PM | Dataset Last Updated: April 23, 2025
Wall pressure data acquired during flight tests at three flight conditions are provided: 48k feet altitude at Mach 0.86; 32k feet at Mach 0.70; and 24k feet at Mach 0.56. Details of the flight test, sensors, and sensor locations are given in a journal article that is referenced in the supporting documents datafile.

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