Flow Characterization of the UTSA Hypersonic Ludwieg Tube

Flow Characterization of the UTSA Hypersonic Ludwieg Tube

The characterization of a hypersonic impulse facility is performed using a variety of methods including Pitot probe scans, particle image velocimetry, and schlieren imaging to verify properties such as the velocity, Mach number, wall boundary layer thickness, and freestream turbulence intensity leve...

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Bibliographic Details
Main Authors: Eugene N. A. Hoffman, Elijah J. LaLonde, Angelina Andrade, Ivana Chen, Hayden A. Bilbo, Christopher S. Combs
Format: Article
Language:English
Published: MDPI AG 2023-05-01
Series:Aerospace
Subjects:
Ludwieg tube
wind tunnel
hypersonics
characterization
particle image velocimetry (PIV)
Online Access:https://www.mdpi.com/2226-4310/10/5/463

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