EXPERIMENTAL MEASUREMENTS OF OBLIQUE SHOCK INDUCED REACTIONS IN HYPERSONIC WEDGE FLOW

von Rosato, Daniel A.
Veröffentlicht in AIAA Propulsion and Energy Forum (2020 : Online) Pressure gain combustion (2020)

SHOCK-INDUCED HIGH-SPEED REACTIONS IN HIGH ENTHALPY HYPERSONIC FLOW

von Sosa, Jonathan
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Pressure gain combustion (2020)

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)

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)

EFFECTS OF DETONATION DECOUPLING ON THE IGNITION OF A SUPERSONIC CAVITY SCRAMJETS

von Rosato, Daniel A.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) High-speed air-breathing propulsion (2020)