Design and Initial Characterization of the UTSI Mach 7 Ludwieg Tube
Author:
Affiliation:
1. The University of Tennessee Space Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1457
Reference19 articles.
1. Calibration of an Actively Controlled Expansion Hypersonic Wind Tunnel
2. The Mach 6 Quiet Tunnel at Texas A&M: Quiet Flow Performance
3. Review of Basic Research and Development Programs Conducted in the LENS Facilities in Hypersonic Flows
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2. Flow Characterization of the UTSA Hypersonic Ludwieg Tube;Aerospace;2023-05-16
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