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Flame structure transition and instability excitation by pilot fuel in a centrally staged combustor
The Physics of FluidsThe pilot stage plays a crucial role in central-staged combustion technology. This study aimed to investigate the impact of the jet-type pilot stage on the flame structure and combustion instability in a novel strong coupled centrally staged swirl gas ...
Pengfei Fu +5 more
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Flame Structure of Ammonium-Dinitramide-Based Liquid Propellant in a Small Thruster
Journal of Propulsion and Power, 2018In this paper, the flame structure of a liquid propellant ammonium dinitramide–methanol aqueous solution in a small model thruster is investigated.
L. Jing +4 more
semanticscholar +1 more source
Laminar hydrocarbon flame structure
Combustion, Explosion, and Shock Waves, 2009From the very first experimental studies, based essentially on flame propagation velocity and flame emission measurements, successive improvements in analytical and numerical techniques have contributed to make the analysis of laminar flame structure a powerful tool for extending the knowledge on combustion chemistry, thermodynamics, and transport ...
C. Vovelle, J. -L. Delfau, L. Pillier
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ACS Applied Materials and Interfaces
Biobased-functionalized metal-organic frameworks (Bio-FUN-MOFs) stand out from the crowd of candidates in the flame-retardant field due to their multipathway flame-retardant mechanisms and green synthesis processes.
Kunpeng Song +8 more
semanticscholar +1 more source
Biobased-functionalized metal-organic frameworks (Bio-FUN-MOFs) stand out from the crowd of candidates in the flame-retardant field due to their multipathway flame-retardant mechanisms and green synthesis processes.
Kunpeng Song +8 more
semanticscholar +1 more source
Symposium (International) on Combustion, 1998
Quantitative CN, OH, and OH rotational temperature, and velocity two-dimensional profiles have been imaged using planar laser-induced fluorescence (PLIF) imaging or particle-imaging velocimetry (PIV) during ignition and deradiative extinguishment of cyclotrimethylene-trimitramine, (RDX) at three different heat flux levels.
Tim Parr, Donna Hanson-Parr
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Quantitative CN, OH, and OH rotational temperature, and velocity two-dimensional profiles have been imaged using planar laser-induced fluorescence (PLIF) imaging or particle-imaging velocimetry (PIV) during ignition and deradiative extinguishment of cyclotrimethylene-trimitramine, (RDX) at three different heat flux levels.
Tim Parr, Donna Hanson-Parr
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Counterflow heptane flame structure
Proceedings of the Combustion Institute, 2000Results are reported for thermocouple and gas-chromatographic measurements of profiles of temperature and of concentrations of C 7 H 16 , C 5 H 10 , C 4 H 8 , C 4 H 6 , C 3 H 6 , C 2 H 6 , C 2 H 4 , C 2 H 2 , CH 4 , CO, and CO 2 in two laminar counterflow n -heptane flames having measured flame temperature of 2100 K, at an oxidizerside potential-flow
S.C. Li, F.A. Williams
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Solid Propellant Flame Structure
MRS Proceedings, 1995AbstractPlanar Laser Induced Fluorescence (PLIF), UV/Vis Absorption, and thermocouple measurements were done for HNF, RDX, HMX, and XM39 deflagration with and without CO2 laser-support. RDX and especially HNF have very short self-deflagration flame length scales. HMX and XM39 have taller self-deflagration flames.
T. P. Parr, D. M. Hanson-Parr
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Chlorine-fluorine flame structure
Symposium (International) on Combustion, 1971Chlorine-fluorine flame, determining adiabatic propagation speed, refractive index field, temperature profile, composition distribution and atom ...
Lawrence L. Ambs, Edward A. Fletcher
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1992
The state-of-the-art in modelling laminar flames is reviewed in three selected areas, viz., (i) derivation of systematically reduced mechanisms, (ii) asymptotic approaches to investigate the structure of steady flames, and, (iii) numerical approaches to the computation of unsteady flames. For each of these topics representative examples are discussed.
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The state-of-the-art in modelling laminar flames is reviewed in three selected areas, viz., (i) derivation of systematically reduced mechanisms, (ii) asymptotic approaches to investigate the structure of steady flames, and, (iii) numerical approaches to the computation of unsteady flames. For each of these topics representative examples are discussed.
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1992
C. K. Law addressed the issue of discrepancies between numerical simulations and experimental observations. He pointed out that simulations employ kinetic and thermal data which are known only approximately. Likewise, experimental data, as recorded, may not conform strictly to conditions experienced by the flame.
A. Kapila, M. Matalon
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C. K. Law addressed the issue of discrepancies between numerical simulations and experimental observations. He pointed out that simulations employ kinetic and thermal data which are known only approximately. Likewise, experimental data, as recorded, may not conform strictly to conditions experienced by the flame.
A. Kapila, M. Matalon
openaire +1 more source

