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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.
Complete Metadata
| bureauCode |
[ "026:00" ] |
|---|---|
| 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 |
| programCode |
[ "026:001" ] |
| theme |
[ "Aerospace" ] |
