Ignition characterization of LOX/hydrocarbon propellants [PDF]
The results of an evaluation of the ignition characteristics of the gaseous oxygen (Gox)/Ethanol propellant combination are presented. Ignition characterization was accomplished through the analysis, design, fabrication and testing of a spark initiated ...
Lawver, B. R. +2 more
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Numerical study of different shape design of piston bowl for diesel engine combustion in a light duty single-cylinder engine. [PDF]
Heliyon, 2022 Deresso H +3 more
europepmc +1 more source
Injector element characterization methodology [PDF]
Characterization of liquid rocket engine injector elements is an important part of the development process for rocket engine combustion devices. Modern nonintrusive instrumentation for flow velocity and spray droplet size measurement, and automated ...
Cox, George B., Jr.
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Vortex cooled thermoplastic chamber thruster for potential application to polymer based 3D printed space propulsion systems. [PDF]
Sci RepAqailan M, Huh J.
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Spray Characteristics of Closed-type Swirl Injectors with Varying Swirl Chamber Geometry
Journal of the Korean Society of Propulsion Engineers, 2015 Yunjae Chung +3 more
openaire +2 more sources
Laboratory measurements in a turbulent, swirling flow [PDF]
Measurements of soot inside a flame-tube burner using a special water-flushed probe are discussed. The soot is measured at a series of points at each burner, and upon occasion gaseous constitutents NO, CO, hydrocarbons, etc., were also measured.
Hoult, D. P.
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Optimization of selective catalytic reduction for nox emission control: an experimental and CFD analysis of mixer designs. [PDF]
Sci RepBandaru S +7 more
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Integrating properties and conditions to predict spray performance of alternative aviation fuel by ANN model. [PDF]
Biotechnol Biofuels Bioprod, 2023 Liu Z, Tang Z, Yang X.
europepmc +1 more source
Near-Field Mixing in a Coaxial Dual Swirled Injector. [PDF]
Flow Turbul CombustMarragou S +3 more
europepmc +1 more source
Predictions and measurements of isothermal flowfields in axisymmetric combustor geometries [PDF]
Numerical predictions, flow visualization experiments and time-mean velocity measurements were obtained for six basic nonreacting flowfields (with inlet swirl vane angles of 0 (swirler removed), 45 and 70 degrees and sidewall expansion angles of 90 and ...
Lilley, D. G., Rhodes, D. L.
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