Results 31 to 40 of about 22,484 (217)
Journal of Thermal Science and Technology, 2012 Combustion oscillation of a self-excited combustion-acoustic phenomenon occurs inside the gas turbine combustor. In general, excessive pressure fluctuation of combustion oscillation may impair the gas turbine engine operation and may result in hardware ...
Kazufumi IKEDA +3 more
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Study of Flow Field Inside a Can Combustor for Micro Gas Turbine Engine Under Nonreacting Flow Conditions [PDF]
Journal of Aerospace Technology and Management, 2021 Generally, micro gas turbines are in the range of 15 to 300 kW. However, recent applications in unmanned aerial vehicles (UAVs) and polygeneration require a small micro gas turbine.
Kirubakaran Vijayakumar, David Bhatt
doaj
Assessment of Combustor Working Environments [PDF]
International Journal of Aerospace Engineering, 2012 In order to assess the remaining life of gas turbine critical components, it is vital to accurately define the aerothermodynamic working environments and service histories. As a part of a major multidisciplinary collaboration program, a benchmark modeling on a practical gas turbine combustor is successfully carried out, and the two-phase, steady ...
Jiang, L., Corber, A.
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Effect of Rotating Direction on Flow and Temperature Field of Concentric Staged Combustor
Xibei Gongye Daxue Xuebao, 2020 The characteristic of cold/reaction flow and temperature field were investigated by using the numerical simulation for concentric staged multi-point direct injection combustor.
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Energies, 2021 HVAF (High Velocity Air Flame) flame spraying can generate supersonic high-temperature gas jets, enabling thermal spraying at unprecedented speeds. However, there is a problem with the energy cost of this device.
Hideo Kawahara +4 more
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Staged combustion concept for gas turbines
Journal of the Global Power and Propulsion Society, 2017 Gas turbine power plants with high load flexibility are particularly suitable to compensate power fluctuations of wind and solar plants. Conventional gas turbines suffer from higher emissions at low load operation.
Dieter Winkler +5 more
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Investigation of the Flow In Cold Condition at the Exit of a Supersonic Combustor Test Bench [PDF]
Journal of Aerospace Technology and Management, 2020 For studies of hypersonic flows and supersonic combustion in ground test facilities, three devices can be used as ram accelerators, shock tunnels and supersonic combustor test benches.
Jefte da Silva Guimarães +3 more
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A novel vortex-fluidized bed combustor with two combustion chambers for rice-husk fuel [PDF]
Songklanakarin Journal of Science and Technology (SJST), 2004 A novel vortexing-fluidized bed combustor (VFBC) using rice-husk as fuel was developed and presented. The combined characteristics of vortex combustion and fluidized bed combustion are the main features of the VFBC, which was designed to achieve high ...
Madhiyanon, T. +2 more
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Unsteady behaviour of opposite impinging jets interaction in crossflow
Nihon Kikai Gakkai ronbunshu, 2016 A mixing of fuel with air in jet engine is studied by analyzing unsteady turbulent flow in a simplified flow channel which consists of the opposed jets in a cross-flow.
Takahisa NAGAO, A.Koichi HAYASHI
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Combustor design and analysis using the ROCket Combustor InteractiveDesign (ROCCID) Methodology [PDF]
26th Joint Propulsion Conference, 1990 The ROCket Combustor Interactive Design (ROCCID) Methodology is a newly developed, interactive computer code for the design and analysis of a liquid propellant rocket combustion chamber. The application of ROCCID to design a liquid rocket combustion chamber is illustrated.
MARK KLEM, JERRY PIEPER, RICHARD WALKER
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