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.
Authors
- Thomas Corke (ORCID: https://orcid.org/0000-0001-8980-1100)
- A. J. M. Spencer (ORCID: https://orcid.org/0000-0002-5673-0921)
- W. K. Jordan (ORCID: https://orcid.org/0000-0001-9105-7376)
- Eric Matlis
- Jacob M. Caldwell
- Alec C. Jobbins
Institutions
- University of Notre Dame (US)
- Notre Dame College (US)
- Notre Dame University (PH)
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