Velocity measurements in a hypersonic flow using acetone molecular tagging velocimetry

A Andrade, ENA Hoffman, EJ LaLonde, CS Combs - Optics Express, 2022 - opg.optica.org
In the present work, a non-intrusive diagnostic technique known as molecular tagging
velocimetry was used to collect quantitative freestream velocity measurements in the Mach 7 …

Measurements of T5 shock tunnel freestream temperature, velocity, and composition

PM Finch, JJ Girard, T Schwartz, CL Strand… - AIAA Journal, 2023 - arc.aiaa.org
We report on measurements of rotational and vibrational temperature, velocity, and
concentrations of nitric oxide (NO) in freestream flows at the T5 reflected shock tunnel at …

Characterization of the T5 reflected shock tunnel freestream temperature, velocity, and composition using laser absorption spectroscopy

J Girard, PM Finch, T Schwartz, W Yu… - AIAA Propulsion and …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-3525. vid We report on
measurements of rotational and vibrational temperature, velocity, and concentrations of nitric …

Development of two-point focused laser differential interferometry for applications in high-speed wind tunnels

A Ceruzzi - 2022 - search.proquest.com
Focused laser differential interferometry (FLDI) and its relative two-point focused laser
differential interferometry (2pFLDI) are completely non-intrusive (ie seedless) optical …

On aerobreakup in the stagnation region of high-Mach-number flow over a bluff body

AR Dworzanczyk, M Viqueira-Moreira… - Journal of Fluid …, 2025 - cambridge.org
In this paper, aerobreakup in the stagnation region of high-Mach-number flow over a bluff
body is studied with experiments and computations. Water drops of diameter 0.51–2.30 mm …

Profiles of streamwise velocity and fluctuations in a hypersonic turbulent boundary layer using acetone tagging velocimetry

BA Segall, D Shekhtman, A Hameed, JH Chen… - Experiments in …, 2023 - Springer
Acetone tagging velocimetry (ATV) with nominally 1% mole fraction acetone seeding was
conducted in a shock-tunnel-generated hypersonic turbulent boundary layer over a hollow …

O2 based resonantly ionized photoemission thermometry analysis of supersonic flows

W McCord, M Gragston, D Plemmons, Z Zhang - Optics Express, 2022 - opg.optica.org
Characterization of the thermal gradients within supersonic and hypersonic flows is
essential for understanding transition, turbulence, and aerodynamic heating. Developments …

Hypersonic boundary-layer instability on a highly cooled cone. Part I: Q-FLDI measurement and instability calculations

A Hameed, D Shekhtman, N Parziale… - AIAA Scitech 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0734. vid In this paper, a Q-FLDI
system was constructed to correlate disturbances inside and outside of the boundary layer …

100 kHz high-spectral-resolution NO-PLIF measurements for compressible flows

NS Rodrigues, PM Danehy, N Jiang, P Hsu… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0405. vid In the present work, we
use a burst-mode laser and optical parametric oscillator system to perform high-spectral …

Two-photon cross-section calculations for krypton in the 190–220 nm range

D Shekhtman, MA Mustafa, NJ Parziale - Applied Optics, 2020 - opg.optica.org
This paper presents multi-path, two-photon excitation cross-section calculations for krypton,
using first-order perturbation theory. For evaluation of the two-photon-transition matrix …