Numerical Investigation of the Effect of Inflow Mach Number on Fuel Mixing in a Supersonic Cavity Combustor

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

IGNITION CRITERIA FOR OBLIQUE DETONATION WAVES IN A HYDROGEN-AIR PREMIXED FREESTREAM

von Bachman, Christian L.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Pressure gain combustion (2021)

WEDGE-STABILIZED OBLIQUE DETONATION WAVES IN A HYPERSONIC HYDROGEN-AIR PREMIXED FREESTREAM

von Bachman, Christian L.
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Pressure gain combustion (2019)

ETHYLENE COMBUSTION IN AN AXISYMMETRIC MACH 4.5 CAVITY

von Hyde, Evan W.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) High-speed air-breathing propulsion (2021)

SYNTHETIC FREESTREAM TURBULENCE GENERATION AT AN INFLOW BOUNDARY CONDITION

von Goodwin, Gabriel B.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Fluid dynamics ; Volume 6 of 6 (2021)

The Influence of Chemical Reaction Models on Combustion Dynamics in an Opposed-Flow Solid Fuel Burner

von DeBoskey, Ryan D.
Veröffentlicht in AIAA SciTech Forum (2023 : National Harbor, Md.; Online) Propellants and combustion ; Volume 1 of 3 (2023)

EVALUATION OF DROPLET AERODYNAMIC BREAKUP MODELS IN SUPERSONIC AND HYPERSONIC FLOWS

von Hess, Andrew
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Fluid dynamics ; Volume 2 of 6 (2021)

CHARACTERIZATION OF SUPERSONIC WIND TUNNEL FLOW QUALITY USING PLANAR LASER CO2 RAYLEIGH SCATTERING

von Munoz, Camilo Aguilera
Veröffentlicht in AIAA Propulsion and Energy Forum (2021 : Online) High-speed air-breathing propulsion (2021)