Calibration of a Mach 5 Ludwieg tube at the University of Arizona

Kyle P. Bearden, Victor E. Padilla, Lutz Taubert, Stuart A. Craig

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

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.

Original languageEnglish (US)
Title of host publicationAIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106101
DOIs
StatePublished - 2021
EventAIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021 - Virtual, Online
Duration: Aug 2 2021Aug 6 2021

Publication series

NameAIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021

Conference

ConferenceAIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021
CityVirtual, Online
Period8/2/218/6/21

ASJC Scopus subject areas

  • Aerospace Engineering
  • Energy Engineering and Power Technology
  • Nuclear Energy and Engineering

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