Flow characterization of the UTSA hypersonic Ludwieg tube

ENA Hoffman, EJ LaLonde, A Andrade, I Chen… - Aerospace, 2023 - mdpi.com
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 …

Hypersonic FLEET velocimetry and uncertainty characterization in a tripped boundary layer

JC Pehrson, BS Leonov, K Melone… - Measurement …, 2023 - iopscience.iop.org
Femtosecond laser electronic excitation tagging (FLEET) velocimetry is applied in a
hypersonic boundary layer behind an array of turbulence-inducing trips. One-dimensional …

Wall-normal fleet velocimetry in a canonical hypersonic inlet

JC Pehrson, BS Leonov, RB Miles… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0220. vid Femtosecond laser
electronic excitation tagging (FLEET) was applied to velocimetry on a hypersonic double-fin …

Hypersonic tripped boundary layer measurements using FLEET velocimetry

JC Pehrson, BS Leonov, RB Miles, C Limbach… - AIAA AVIATION 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-3477. vid Femtosecond laser
electronic excitation tagging was applied in a transitioning boundary layer behind an array …