STUDY OF OBLIQUE SHOCK INDUCED REACTIONS AT MODERATE TOTAL TEMPERATURES

von Rosato, Daniel A.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Pressure gain combustion (2021)

DESIGN AND CHARACTERIZATION OF MACH 5 FLOW FOR HIGHLY TURBULENT HYPERSONIC TEST FACILITY

von Thornton, Mason R.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Ground testing (2021)

FUEL DISTRIBUTION MEASUREMENTS IN A HYPERSONIC COMBUSTOR FACILITY

von Rosato, Daniel A.
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) High-speed air-breathing propulsion (2021)

Comparison and Analysis of Hypersonic Scramjet Nozzles

von Moizes, Dustyn A. Vianna
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Inlets, nozzles, and propulsion systems integration (2023)

CFD Analysis of Scramjet Fuel Injectors

von Sprunger, Justin D.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) High-speed air-breathing propulsion (2023)

Variable Busemann Inlet Geometries for Hypersonic Vehicles

von Clemence, Laurel K.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Inlets, nozzles, and propulsion systems integration (2023)

Experimental Study of Oblique Detonation Wave Stabilization on a Wedge

von White, Zachary P.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Pressure gain combustion (2023)