Supersonic combustion in air-breathing propulsion systems for hypersonic flight
J Urzay - Annual Review of Fluid Mechanics, 2018 - annualreviews.org
Great efforts have been dedicated during the last decades to the research and development
of hypersonic aircrafts that can fly at several times the speed of sound. These aerospace …
of hypersonic aircrafts that can fly at several times the speed of sound. These aerospace …
LES for supersonic combustion
C Fureby - 18th AIAA/3AF international space planes and …, 2012 - arc.aiaa.org
This paper describes the state-of-the-art in Large Eddy Simulation (LES) of supersonic
combustion with application to ram and scramjet engines. Some background is provided …
combustion with application to ram and scramjet engines. Some background is provided …
Incipient thermal choking and stable shock-train formation in the heat-release region of a scramjet combustor. Part II: Large eddy simulations
The flow in the HyShot II scramjet combustor is studied using large eddy simulations (LES).
The computations are made feasible by two important modeling ingredients: an equilibrium …
The computations are made feasible by two important modeling ingredients: an equilibrium …
Large-eddy/Reynolds-averaged Navier–Stokes simulation of cavity-stabilized ethylene combustion
AS Potturi, JR Edwards - Combustion and Flame, 2015 - Elsevier
In this study, a hybrid large-eddy/Reynolds-averaged Navier–Stokes (LES/RANS) method is
used to simulate ethylene combustion inside a cavity flameholder. The cavity flameholder …
used to simulate ethylene combustion inside a cavity flameholder. The cavity flameholder …
Understanding scramjet combustion using LES of the HyShot II combustor
K Nordin-Bates, C Fureby, S Karl… - Proceedings of the …, 2017 - Elsevier
Detailed understanding of the physical processes occurring in the combustor of a scramjet
engine is crucial for enabling this technology and is considered the most promising for …
engine is crucial for enabling this technology and is considered the most promising for …
Large-eddy/Reynolds-averaged Navier–Stokes simulations of reactive flow in dual-mode scramjet combustor
JA Fulton, JR Edwards, HA Hassan… - Journal of Propulsion …, 2014 - arc.aiaa.org
Numerical simulations of the turbulent reactive flow within a model scramjet combustor
configuration, experimentally mapped at the University of Virginia's Scramjet Combustion …
configuration, experimentally mapped at the University of Virginia's Scramjet Combustion …
Dual-pump coherent anti-stokes raman spectroscopy measurements in a dual-mode scramjet
In this paper, the authors describe dual-pump coherent anti-Stokes Raman spectroscopy
(CARS) measurements of mixing and combustion in a direct-connect scramjet combustor …
(CARS) measurements of mixing and combustion in a direct-connect scramjet combustor …
Nonequilibrium supersonic freestream studied using coherent anti-Stokes Raman spectroscopy
Measurements were conducted at the University of Virginia Supersonic Combustion Facility
of the flow in a constant-area duct downstream of a Mach 2 nozzle. The airflow was heated …
of the flow in a constant-area duct downstream of a Mach 2 nozzle. The airflow was heated …
OH PLIF visualization of the UVa supersonic combustion experiment: Configuration A
Hydroxyl radical (OH) planar laser-induced fluorescence (PLIF) visualizations were
performed in the University of Virginia supersonic combustion experiment. The test section …
performed in the University of Virginia supersonic combustion experiment. The test section …
Hybrid Large-Eddy/Reynolds-averaged Navier–Stokes simulations of flow through a model scramjet
AS Potturi, JR Edwards - AIAA journal, 2014 - arc.aiaa.org
The reactive flow through a model scramjet combustor is simulated using a hybrid large-
eddy/Reynolds-averaged Navier–Stokes technique. The scramjet configuration considered …
eddy/Reynolds-averaged Navier–Stokes technique. The scramjet configuration considered …