Velocity and temperature measurements in Mach 18 nitrogen flow at Tunnel 9

A Dogariu, LE Dogariu, MS Smith… - AIAA Scitech 2021 …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-0020. vid We report the first
application of Femtosecond Laser Electronic Excitation Tagging (FLEET) and Coherent Anti …

Hypersonic wake measurements behind a slender cone using FLEET velocimetry

Y Zhang, DR Richardson, SJ Beresh… - AIAA aviation 2019 …, 2019 - arc.aiaa.org
Femtosecond Laser Electronic Excitation Tagging (FLEET) is a velocimetry method that
takes advantage of naturally present nitrogen for flow tagging [1]. Initially developed in …

100 kHz PLEET velocimetry in a Mach-6 Ludwieg tube

PS Hsu, N Jiang, JS Jewell, JJ Felver, M Borg… - Optics …, 2020 - opg.optica.org
Picosecond laser electronic-excitation tagging (PLEET) was demonstrated in a Mach-6
Ludwieg tube at a repetition rate of 100 kHz using a 1064 nm, 100 ps burst-mode laser. The …

Non-intrusive measurement techniques for flow characterization of hypersonic wind tunnels

PM Danehy, J Weisberger, C Johansen, D Reese… - 2018 - ntrs.nasa.gov
This manuscript describes the wide variety of optical measurement techniques for
characterizing the flow in hypersonic wind tunnels. The introduction briefly describes …

Mach 18 flow velocimetry with 100-kHz KTV and PLEET in AEDC Tunnel 9

N Jiang, PS Hsu, SW Grib, M Slipchenko… - Applied Optics, 2023 - opg.optica.org
Krypton Tagging Velocimetry (KTV) and Picosecond Laser Electronic Excitation Tagging
(PLEET) velocimetry at a 100-kHz rate were demonstrated in Mach 18 flow conditions at the …

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 N2 boundary layer flow velocity profile measurements using FLEET

JL Hill, PS Hsu, N Jiang, SW Grib, S Roy, M Borg… - Applied Optics, 2021 - opg.optica.org
Femtosecond laser electronic excitation tagging (FLEET) velocimetry was used in the
boundary layer of an ogive-cylinder model in a Mach-6 Ludwieg tube. One-dimensional …

Implementation of self-aligned focusing Schlieren for hypersonic boundary layer measurements

JL Hill, MP Borg, EK Benitez, CL Running… - AIAA SciTech 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-2438. vid A self-aligned focusing
schlieren (SAFS) apparatus based on a recently published design is implemented for the …

Flow characterization at heated air supersonic facility sbr-50

P Andrews, P Lax, S Elliott, A Firsov, S Leonov - Fluids, 2022 - mdpi.com
The supersonic wind tunnel facility SBR-50 at the University of Notre Dame was built in 2015
for experimental research related to shock wave (SW) interactions with obstacles and …

基于飞秒激光电子激发标记测速技术的剪切流场速度测量

杨文斌, 陈力, 闫博, 王朝宗, 周江宁, 陈爽… - 实验流体 …, 2022 - pubs.cstam.org.cn
流场速度测量精度会影响飞行器气动性能的预测精度, 常用的基于激光技术的非接触式速度测量
方法已不能完全满足流场速度高精度测量需求, 飞秒激光电子激发标记(Femtosecond Laser …