Global reconstruction of hypersonic boundary layer disturbance modes

JL Hill, EK Benitez, MP Borg, MF Reeder - AIAA SciTech 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0869. vid The reconstruction of
globally-consistent hypersonic boundary layer disturbance modes from experimental …

Self-aligned focusing schlieren in optically constrained environments

BF Bathel, MT Boyda, JM Weisberger - Applied Optics, 2024 - opg.optica.org
A method is presented to acquire self-aligned focusing schlieren (SAFS) images when the
optical axis of the instrument is positioned at a non-normal incidence angle to the …

Separation and Transition on the ROTEX-T Cone-Flare

J Davami, TJ Juliano, A Scholten, P Paredes… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
As part of NATO STO AVT-346 “Predicting Hypersonic Boundary-Layer Transition on
Complex Geometries,” coordinated experimental and computational studies were conducted …

Colinear focused laser differential interferometry and self-aligned focusing schlieren

JM Weisberger, BF Bathel - Applied Optics, 2023 - opg.optica.org
A colinear focused laser differential interferometer (FLDI) and self-aligned focusing schlieren
(SAFS) system has been assembled and tested in the laboratory, using a turbulent jet of …

[HTML][HTML] Application of high-speed self-aligned focusing schlieren system for supersonic flow velocimetry

PA Lax, SB Leonov - Aerospace, 2024 - mdpi.com
A self-aligned focusing schlieren (SAFS) system combines the field of view of a conventional
schlieren system with the defocus blur of a focusing schlieren system away from the object …

Leading-edge curvature influence on hypersonic boundary layer transition

JL Hill, MP Borg, MW Tufts, EK Benitez… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0098. vid A series of experiments
were performed in the Air Force Research Laboratory Mach-6 Ludwieg Tube using a …

Nosetip bluntness effects on a cone-cylinder-flare at mach 6

EK Benitez, MP Borg, JL Hill - Experiments in Fluids, 2024 - Springer
A cone-cylinder-flare model with sharp and blunt nosetips was tested at the AFRL Mach-6
Ludwieg Tube at a 0\(^{\circ}\) angle of attack. Surface-pressure fluctuation measurements …

Effect of porosity on the ability of silicon-carbide foams to attenuate second-mode boundary-layer instability

BL Bemis, MC Sieve, JL Hill, MP Borg… - AIAA AVIATION 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-3706. vid This work experimentally
investigated the second-mode boundary-layer instability over four different material inserts …

Development and characterization of high Mach nozzle using high-frequency optical and surface techniques

N Kiefer, J Braun, G Paniagua - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
Low and high-frequency surface techniques characterized a Mach 4 to 6 nozzle with an
accelerating boundary layer. Schlieren imaging was used to describe the starting behavior …

Development of a fs/ps CARS system for temperature measurements in supersonic and hypersonic environments

A Stevenson, CE Dedic, NS Rodrigues… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
A hybrid femtosecond/picosecond coherent anti-Stokes Raman scattering (fs/ps CARS)
system was developed for quantitative measurements of temperature in a laboratory-scale …