FLOW QUALITY MAPPING OF THE MACH 4 QUIET LUDWIEG TUBE

von Flood, John T.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Fluid dynamics ; Volume 2 of 7 (2020)

FIRST AND MACK-MODE INSTABILITIES IN A FLAT-PLATE BOUNDARY LAYER AT MATCH 4

von Flood, John T.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Fluid dynamics ; Volume 2 of 7 (2020)

CALIBRATION OF A MACH 5 LUDWIEG TUBE AT THE UNIVERSITY OF ARIZONA

von Bearden, Kyle P.
Veröffentlicht in AIAA Aviation Forum (2021 : Online) Ground testing (2021)

Experimental Measurements and Numerical Investigations of Boundary-Layer Instabilities on a Mach 5 Hollow Cylinder

von Flood, John J.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Fluid dynamics ; Volume 4 of 6 (2023)

FLOW STRUCTURE AND HEAT TRANSFER CHARACTERIZATION OF A BLUNT-FIN- INDUCED SHOCK-WAVE/LAMINAR BOUNDARY-LAYER INTERACTION

von Maldonado, Jorge Castro
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Fluid dynamics ; Volume 4 of 6 (2021)

Fin-Induced Shock Boundary Layer Interactions on a Flat Plate and Hollow Cylinder at Mach 5

von Threadgill, James A.
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Fluid dynamics ; Volume 6 of 7 (2022)

DEVELOPMENT OF PLASMA-BASED CONTROLLED DISTURBANCES FOR THE STUDY OF BOUNDARY LAYER TRANSITION AND SHOCK BOUNDARY LAYER INTERACTION

von Singh, Ashish
Veröffentlicht in AIAA Aviation Forum (2021 : Online) Fluid dynamics ; Volume 1 of 2 (2021)