Results 11 to 20 of about 22,484 (217)

Prediction of Liner Metal Temperature of an Aeroengine Combustor with Multi-Physics Scale-Resolving CFD

open access: yesEntropy, 2021
Computational Fluid Dynamics is a fundamental tool to simulate the flow field and the multi-physics nature of the phenomena involved in gas turbine combustors, supporting their design since the very preliminary phases.
Davide Bertini   +2 more
doaj   +1 more source

Alternate-Fueled Combustor-Sector Performance—Part A: Combustor Performance and Part B: Combustor Emissions [PDF]

open access: yesISRN Mechanical Engineering, 2012
Alternate aviation fuels for military or commercial use are required to satisfy MIL-DTL-83133F or ASTM D 7566 standards, respectively, and are classified as “drop-in’’ fuel replacements. To satisfy legacy issues, blends to 50% alternate fuel with petroleum fuels are acceptable.
D. T. Shouse   +7 more
openaire   +1 more source

Improving Blowout Performance of the Conical Swirler Combustor by Employing Two Parts of Fuel at Low Operating Condition

open access: yesEnergies, 2021
Aiming at the problem of the narrow combustion stability boundary, a conical swirler was designed and constructed based on the concept of fuel distribution.
Yixiang Yuan   +5 more
doaj   +1 more source

Small gas turbine combustor study - Combustor liner evaluation [PDF]

open access: yes21st Aerospace Sciences Meeting, 1983
A reverse flow combustor liner constructed of Lamilloy (a multilaminate transpiration type material) is compared both analytically and experimentally with a conventional splash film-cooled design with the same combustor configuration. Comparison of selected critical combustor panels indicated that it was possible to maintain the liner temperature ...
C. NORGREN, S. RIDDLEBAUGH
openaire   +1 more source

Application of a three-step approach for prediction of combustion instabilities in industrial gas turbine burners

open access: yesJournal of the Global Power and Propulsion Society, 2018
Recently, because of environmental regulations, gas turbine manufacturers are restricted to produce machines that work in the lean combustion regime. Gas turbines operating in this regime are prone to combustion-driven acoustic oscillations referred as ...
Dmytro Iurashev   +5 more
doaj   +1 more source

Experimental and Simulation Study on the Emissions of a Multi-Point Lean Direct Injection Combustor [PDF]

open access: yesJournal of Applied Fluid Mechanics, 2023
Spurred by the world’s attention to pollution emissions from commercial aero-engines, the International Civil Aviation Organization (ICAO) has made more stringent emission regulations for civil aircraft engines, especially the NOx emission.This paper ...
P. Zhu   +5 more
doaj   +1 more source

Aerothermal Performance and Soot Emissions of Reacting Flow in a Micro-Gas Turbine Combustor

open access: yesEnergies, 2023
Micro-gas turbines are used for power generation and propulsion in unmanned aerial vehicles. Despite the growing demand for electric engines in a world striving for a net zero carbon footprint, combustion gas turbines will continue to play a critical ...
Heyu Wang, Kai Hong Luo
doaj   +1 more source

A Real-Time Combustion Instability Simulation with Comprehensive Thermo-Acoustic Dynamic Model

open access: yesEnergies, 2018
The thermo-acoustic instability in the combustion process of a gas turbine is caused by the interaction of the heat release mechanism and the pressure perturbation.
Jaeyoung Han   +3 more
doaj   +1 more source

Flame stability and behavior inside meso-scale combustor with different flame holder

open access: yesMATEC Web of Conferences, 2018
Flame stability and behavior inside meso-scale combustor with different flame holder was investigated experimentally. Three types of flame holder i.e. wire mesh, flat plate with circular holes and flat plate with narrow slits, were used to improve the ...
Yuliati Lilis
doaj   +1 more source

Robust Gas Turbine Combustor with Acoustic Liner

open access: yesJournal of Thermal Science and Technology, 2012
Combustion oscillation of a self-excited thermo-acoustic phenomenon occurs inside the gas turbine combustor. Its excessive pressure fluctuation may impair the gas turbine engine operation, and could result in hardware severe damages.
Kazufumi IKEDA   +2 more
doaj   +1 more source

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