Results 171 to 180 of about 21,213 (234)
Influence of the non-equal aligned nozzles for fuel injection inside the supersonic combustion chamber. [PDF]
Sci RepFan Z +7 more
europepmc +1 more source
Thermodynamics, Environmental and Sustainability Impacts of a Turbofan Engine Under Different Design Conditions Considering Variable Needs in the Aviation Industry. [PDF]
Glob ChallAygun H, Sheikhi MR, Caliskan H.
europepmc +1 more source
Numerical Study of Ignition and Combustion of Hydrogen-Enriched Methane in a Sequential Combustor. [PDF]
Flow Turbul CombustImpagnatiello M, Malé Q, Noiray N.
europepmc +1 more source
A novel strut injector with lateral extruded nozzle for efficient hydrogen mixing in supersonic combustors. [PDF]
Sci RepLajimi RH +7 more
europepmc +1 more source
Coordinated distributed model predictive control for multi energy carrier systems. [PDF]
Sci RepEl-Afifi MI +4 more
europepmc +1 more source
Thermal performance of a micro-combustor for micro-gas turbine system
Energy Conversion and Management, 2007 Premixed combustion of hydrogen gas and air was performed in a stainless steel based micro-annular combustor for a micro-gas turbine system. Micro-scale combustion has proved to be stable in the micro-combustor with a gap of 2 mm.
J L Xu
exaly +2 more sources
Some of the next articles are maybe not open access.
Related searches:
Related searches:
Effects of Combustor Enclosure Flow Path on Combustor Design
Volume 4A: Combustion, Fuels, and Emissions, 2020Abstract A design optimization procedure was implemented to resize the holes of a combustor liner for practical applications. A combustor geometry evaluated without an enclosure was to be reformulated within an enclosure. The objective functions of the combustor with enclosure involved targeting the flow splits of the combustor without ...
Alejandro M. Briones +2 more
openaire +1 more source
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 2009
An investigation is undertaken into the potential use of carbon-carbon materials for Scramjet combustors and configurations utilising regenerative and radiative cooling are considered. The analysis uses the ANSYS package to couple a CFD analysis of the fuel cooling with a structural thermal analysis.
Zander, Fabian, Morgan, Richard
openaire +2 more sources
An investigation is undertaken into the potential use of carbon-carbon materials for Scramjet combustors and configurations utilising regenerative and radiative cooling are considered. The analysis uses the ANSYS package to couple a CFD analysis of the fuel cooling with a structural thermal analysis.
Zander, Fabian, Morgan, Richard
openaire +2 more sources