Measurement Accuracy and Uncertainty Analysis of the X-59 Air Data Probe Calibration Test Entry One

The X-59 is being developed to demonstrate quiet sonic boom technology. Data was obtained via two test entries in the NASA Glenn Research Center’s 8- by 6-Foot Supersonic Wind Tunnel to calibrate the X-59’s nose air data probe. The first entry tested two theoretically identical probes with the inten...

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Bibliographische Detailangaben

Hauptverfasser:	Friedlander, David J., Bozeman, Michael D., Elmiligui, Alaa A., Flamm, Jeffrey D., Mears, Lee J., Winsk, Courtney S., Long, Kurtis R.
Format:	Report
Sprache:	eng
Schlagworte:	Avionics and Aircraft Instrumentation
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