Instability and transition onset downstream of a laminar separation bubble at Mach 6
Instability measurements of an axisymmetric, laminar separation bubble were made over a
sharp cone-cylinder-flare with a flare angle under hypersonic quiet flow. Two distinct …
sharp cone-cylinder-flare with a flare angle under hypersonic quiet flow. Two distinct …
Implementation of self-aligned focusing Schlieren for hypersonic boundary layer measurements
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 …
schlieren (SAFS) apparatus based on a recently published design is implemented for the …
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 …
optical axis of the instrument is positioned at a non-normal incidence angle to the …
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 …
(SAFS) system has been assembled and tested in the laboratory, using a turbulent jet of …
Thermal Evaluation of the Initial Concept 3. X Vehicle at Mach 7
High-speed global surface temperature distributions and heat flux measurements on the
Initial Concept 3. X vehicle (IC3X) model were investigated at the UTSA Mach 7 wind tunnel …
Initial Concept 3. X vehicle (IC3X) model were investigated at the UTSA Mach 7 wind tunnel …
Effects of Surface Roughness on Shock-Wave/Boundary-Layer Interactions at Mach 7.2
ENA Hoffman - 2023 - search.proquest.com
This research work studies the effects of surface roughness on shock-wave/boundary-layer
interactions (SWBLIs). SWBLI are prevalent in supersonic and hypersonic flows and occur …
interactions (SWBLIs). SWBLI are prevalent in supersonic and hypersonic flows and occur …