Design and Characterization of the Notre Dame STEM Mach 6 Ludwieg Tube

The University of Notre Dame has designed and constructed a new Mach 6 Ludwieg tube for the purpose of hypersonics research and education. The tunnel uses a fast acting plunger valve to actuate the flow, providing run times of 55 ms. The Mach 6 flow is generated through a 0.28 meter diameter nozzle. Pitot pressures are measured on the centerline, and with a rake. The nominal Mach number was found to be 5.8 and pitot pressure fluctuations were 1.5 %, both varying with unit Reynolds number. Possible air liquefaction is present at high Reynolds numbers, which is apparent from a rise in noise.

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Publication Details

Published
2025-07-16
DOI
https://doi.org/10.2514/6.2025-3044
Citations
1
Primary Topic
Spacecraft and Cryogenic Technologies
Type
article
Field-Weighted Citation Impact
4.99
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article

Design and Characterization of the Notre Dame STEM Mach 6 Ludwieg Tube

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1 citations
Spacecraft and Cryogenic Technologies
4.99
article

Design and Characterization of the Notre Dame STEM Mach 6 Ludwieg Tube

Thomas Corke, A. J. M. Spencer, W. K. Jordan, Eric Matlis, Jacob M. Caldwell, Alec C. Jobbins
article en
1 citations

Abstract

The University of Notre Dame has designed and constructed a new Mach 6 Ludwieg tube for the purpose of hypersonics research and education. The tunnel uses a fast acting plunger valve to actuate the flow, providing run times of 55 ms. The Mach 6 flow is generated through a 0.28 meter diameter nozzle. Pitot pressures are measured on the centerline, and with a rake. The nominal Mach number was found to be 5.8 and pitot pressure fluctuations were 1.5 %, both varying with unit Reynolds number. Possible air liquefaction is present at high Reynolds numbers, which is apparent from a rise in noise.

University of Notre Dame (US), Notre Dame College (US), Notre Dame University (PH)
Openalex Percentile: Top 5%
Spacecraft and Cryogenic Technologies
4.99
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