Results 71 to 80 of about 2,006 (138)

Continuous Detonation Combustor Operating on a Methane–Oxygen Mixture: Test Fires, Thrust Performance, and Thermal State

open access: yesAerospace
Test fires of a rotating detonation engine (RDE) annular combustor operating on a methane–oxygen mixture were conducted. Compared to the original RDE combustor previously tested, it was modified in terms of changing the layout of the water cooling system,
Sergey M. Frolov   +3 more
doaj   +1 more source

Thermal and Exergy Assessment of a Micro Combustor Fueled by Premixed Hydrogen/Air under Different Sizes: a Numerical Simulation

open access: yesJournal of Applied Fluid Mechanics, 2020
In this work, a numerical study has been carried out in order to investigate the effects of a micro combustor size on the exergy and energy efficiencies of a premixed hydrogen/air for a micro thermophotovoltaic system. For this purpose, six combustors in
E. Nadimi, S. Jafarmadar
doaj  

Three-Dimensional Analysis of a Steam-Injected Gas Turbine Combustor Fuelled by an Ammonia-Hydrogen Blend

open access: yesPolish Maritime Research
This work presents a 3D numerical study of a steam-injected combustor for a gas turbine operating on an ammonia-hydrogen fuel blend, aimed at enabling carbon-free hybrid energy systems. The research focuses on the performance and emission characteristics
Serbin Serhiy   +4 more
doaj   +1 more source

Experimental Study of Ignition Characteristics in Oblique-Injected Annular Combustors Using a Pre-Chamber Ignition System

open access: yesAerospace Research Communications
In this work, a pre-chamber ignition system is used to initiate the ignition in a premixed oblique-injected annular combustor. Although the introduction of the oblique-injecting burner in the gas turbine improved the gyratory flow motion and flow ...
Haroun Hassan   +9 more
doaj   +1 more source

Shock wave enhanced turbulent mixing in a wide-speed-range strut-based scramjet combustor

open access: yesPropulsion and Energy
The efficient mixing of fuel and oxidizer in a scramjet combustor is a critical issue for achieving future wide-speed-range flight. A numerical study is conducted using Reynolds-averaged Navier–Stokes equations coupled with shear stress transport k-ω ...
Xiaofei Niu, Qian Chen
doaj   +1 more source

Research on substitutability of single-dome versus triple-dome center staged combustor

open access: yesCase Studies in Thermal Engineering
To investigate the substitutability of the simulation results using the single-dome combustor as the computational domain to the triple-dome combustor, three-dimensional numerical simulations were conducted on both models and the differences in various ...
Duo Wang   +4 more
doaj   +1 more source

Combustion performance of n-butane-fueled mesoscale annular combustor

open access: yesJournal of Thermal Science and Technology
The lower vapor pressure of n-butane than gaseous fuels, such as hydrogen, methane, and propane, enables its fuel containers to be compact and highly portable.
Yosuke SUENAGA, Hideki YANAOKA
doaj   +1 more source

A deep learning-based approach for flow field prediction in a dual-mode combustor

open access: yesPropulsion and Power Research
Accurate acquisition of the distribution of flow parameters inside the supersonic combustor is of great significance for hypersonic flight control. It is an interesting attempt to introduce a data-driven model to a supersonic combustor for flow field ...
Chen Kong   +4 more
doaj   +1 more source

Investigations of Combustion Performance in LPP Combustor

open access: yesJournal of Applied Fluid Mechanics, 2017
A Lean Premixed Prevaporized (LPP) low-emission combustor which is applied with the combustion technology of staged lean fuel is developed. To study the cold flow dynamics and the combustion performance of the LPP combustor, both experimental tests using
Y. W. Yan, Y. P. Liu, J. H. Li, W. Cai
doaj  

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