SPATIALLY-RESOLVED OPTICAL DETECTION OF JET SCREECH IN A MACH 1.5 UNDEREXPANDED JET WITH FOCUSED-LASER DIFFERENTIAL INTERFEROMETRY

von Price, Theron J.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Aerodynamic measurement technology ; Volume 2 of 2 (2021)

MODAL ANALYSIS OF A MACH 1.5 UNDEREXPANDED JET USING TIME-RESOLVED OPTICAL DIAGNOSTICS

von Price, Theron J.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Fluid dynamics ; Volume 4 of 7 (2020)

Analysis of Screech Phenomena in a Mach 1.0 Jet with Linear Array Focused Laser Differential Interferometry

von Price, Theron J.
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Aerodynamic measurement technology ; Volume 2 of 2 (2022)

Experimental Investigation of a High-Frequency Pulsed Supersonic Co-Axial Injector Using Optical Diagnostics

von Jenkins, Jacob E.
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Fluid dynamics ; Volume 3 of 3 (2023)

DESIGN AND INITIAL CHARACTERIZATION OF THE UTSI MACH 4 LUDWIEG TUBE

von Kreth, Phillip A.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Ground testing (2021)

DYNAMICS OF CYLINDER-INDUCED TRANSITIONAL AND TURBULENT SHOCKWAVE-BOUNDARY LAYER INTERACTIONS ON A 6° CONE AT MACH 4

von Lester, Lauren E.
Veröffentlicht in AIAA Aviation Forum (2021 : Online) Fluid dynamics ; Volume 1 of 2 (2021)

Characterization of Temperature Sensitive Paint for Application in Hypersonic Ludwieg Tubes at the University of Tennesse

von Smith, Cary
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Aerodynamic measurement technology ; Volume 2 of 2 (2022)

Temperature-Sensitive Paint Measurements of Cylinder-Induced Shockwave-Boundary Layer Interaction on a 6-degree Cone with Laminar Mach 7 Flow

von Smith, Cary D.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Aerodynamic measurement technology ; Volume 2 of 2 (2023)

Velocity and Vorticity Fields of a High-Frequency Pulsed Supersonic Co-Axial Injector

von Solomon, John T.
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Fluid dynamics ; Volume 3 of 3 (2023)

Separation Region Unsteadiness Drivers in Swept Compression Ramps

von Allen, Daniel S.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Fluid dynamics ; Volume 6 of 6 (2023)

EXPLORATION OF UPSTREAM INFLUENCE AND THE ROLE OF SHOCK GENERATOR GEOMETRY IN SHOCK WAVE/TRANSITIONAL BOUNDARY LAYER INTERACTIONS AT MACH 1.8 EDGE CONDITIONS

von Lash, E. Lara
Veröffentlicht in AIAA Aviation Forum (2020 : Online) Fluid dynamics ; Volume 2 of 3 (2020)

A Computational and Experimental Investigation into Jet Aeroacoustics for Improved Ground Test Design

von Kreth, Phillip A.
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Aeroacoustics ; Volume 2 of 6 (2023)

Design and Initial Characterization of the UTSI Mach 7 Ludwieg Tube

von Gragston, Mark
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Ground testing (2023)

Analysis of Streamwise Vortex Streaks in Shockwave-Boundary Layer Interactions on a Hollow Cylinder-Flare at M∞ = 4

von Ledbetter, Shelby Y.
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Fluid dynamics ; Volume 1 of 3 (2023)

SIMULATIONS OF DYNAMIC SHOCK WAVE/BOUNDARY LAYER INTERACTIONS USING HPCMP CREATETM-AV KESTREL COFFE

von Nutter, Nicole F.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Fluid dynamics ; Volume 2 of 6 (2021)