Results 11 to 20 of about 27,437 (306)

Analysis of Gaseous and Gaseous-Dusty, Premixed Flame Propagation in Obstructed Passages with Tightly Placed Obstacles

open access: yesFluids, 2020
A recent predictive scenario of premixed flame propagation in unobstructed passages is extended to account for obstructions that can be encountered in facilities dealing with explosive materials such as in coalmines.
Furkan Kodakoglu   +3 more
doaj   +1 more source

Pulsating regimes of flames propagation in a model with chain-branching reaction [PDF]

open access: yesКомпьютерные исследования и моделирование, 2009
In this paper we investigate propagation of planar combustion waves in an adiabatic model with two-step chain branching reaction mechanism. Pulsating instabilities are found to emerge for fuel Lewis number greater than one due to a Hopf bifurcation.
V. V. Gubernov   +2 more
doaj   +1 more source

Transfer learning of deep neural networks for predicting thermoacoustic instabilities in combustion systems

open access: yesEnergy and AI, 2021
The intermittent nature of operation and unpredictable availability of renewable sources of energy (e.g., wind and solar) would require the combustors in fossil-fuel power plants, sharing the same grid, to operate with large turn-down ratios. This brings
Sudeepta Mondal   +3 more
doaj   +1 more source

Experimental Investigation of Flame Anchoring Behavior in a LOX/LNG Rocket Combustor

open access: yesAerospace, 2023
Hot fire tests of a multi-injector research combustor were performed with liquid-oxygen and liquefied-natural-gas (LOX/LNG) propellants at chamber pressures from 30 up to 67 bar, hence at conditions similar to an upper stage rocket engine.
Jan Martin   +4 more
doaj   +1 more source

Numerical Analysis of Self-Excited Combustion Instabilities in a Small MMH/NTO Liquid Rocket Engine

open access: yesInternational Journal of Aerospace Engineering, 2020
Combustion instabilities in a small MMH/NTO liquid rocket engine used for satellite attitude and course control are numerically investigated. A three-dimensional Navier-Stokes code is developed to simulate two-phase spray combustion for cases with five ...
Jianxiu Qin, Huiqiang Zhang
doaj   +1 more source

Effect of ramp-cavity on hydrogen fueled scramjet combustor

open access: yesPropulsion and Power Research, 2014
Sustained combustion and optimization of combustor are the two challenges being faced by combustion scientists working in the area of supersonic combustion.
J.V.S. Moorthy   +3 more
doaj   +1 more source

Some dynamics of acoustic oscillations with nonlinear combustion and noise [PDF]

open access: yes, 1997
The results given in this paper constitute a continuation of progress with nonlinear analysis of coherent oscillations in combustion chambers. We are currently focusing attention on two general problems of nonlinear behavior important to practical ...
Burnley, V. S., Culick, F. E. C.
core   +1 more source

3D convolutional selective autoencoder for instability detection in combustion systems

open access: yesEnergy and AI, 2021
While analytical solutions of critical (phase) transitions in dynamical systems are abundant for simple nonlinear systems, such analysis remains intractable for real-life dynamical systems. A key example is thermoacoustic instability in combustion, where
Tryambak Gangopadhyay   +6 more
doaj   +1 more source

Accounting for convective effects in zero-Mach-number thermoacoustic models [PDF]

open access: yes, 2014
This paper presents a methodology to account for some mean-flow effects on thermo-acoustic instabilities when using the zero-Mach-number assumption. It is shown that when a computational domain is represented under the M=0 assumption, a nonzero-Mach ...
Bloxsidge   +48 more
core   +5 more sources

Cycle-Resolved Computations of Stratified-Charge Turbulent Combustion in Direct Injection Engine

open access: yesJournal of Thermal Science and Technology, 2013
An extremely lean burning engine has been expected to improve fuel consumption rate of engines. To achieve this, stable combustion should be realized for a wide range of operating conditions at air-fuel ratio over 40.0.
Nobuhiro SHINMURA   +2 more
doaj   +1 more source

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