Turbulent boundary layer wall pressure flight data

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.

Data and Resources

Additional Info

Field Value
Maintainer Albert Allen
Last Updated April 23, 2025, 22:37 (UTC)
Created March 31, 2025, 14:01 (UTC)
accessLevel public
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harvest_source_title DNG Legacy Data
identifier https://data.nasa.gov/api/views/5pvz-kbwd
issued 2019-03-04
landingPage https://data.nasa.gov/dataset/turbulent-boundary-layer-wall-pressure-flight-data
modified 2024-05-15
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publisher Albert Allen
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