@inproceedings{922c0f081a4344059565b48c76fff40a,
title = "Calibration of a Mach 5 Ludwieg tube at the University of Arizona",
abstract = "Calibration, commissioning, and design features of a new Mach 5 Ludwieg Tube wind tunnel at the University of Arizona are discussed. Mach-number uniformity and free-stream noise levels are measured using a Pitot rake at a range of unit Reynolds numbers at multiple spanwise and streamwise positions. The wind tunnel is shown to have a free-stream Mach number of 4.82 with variance less than 0.8\% (and less than 0.5\% at most streamwise positions). The average free-stream noise level in the core (based on Pitot measurements) is shown to be less than 1.2\% at an intermediate Reynolds number with some regions dropping locally below 1.0\%. The core flow region is measured to be 282.4 mm (11.1 in) in diameter at the nozzle exit.",
author = "Bearden, \{Kyle P.\} and Padilla, \{Victor E.\} and Lutz Taubert and Craig, \{Stuart A.\}",
note = "Publisher Copyright: {\textcopyright} 2021, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.; AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021 ; Conference date: 02-08-2021 Through 06-08-2021",
year = "2021",
doi = "10.2514/6.2021-2950",
language = "English (US)",
isbn = "9781624106101",
series = "AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021",
}