Results 51 to 60 of about 21,213 (234)
Large Eddy Simulations of gaseous flames in gas turbine combustion chambers [PDF]
, 2012 Recent developments in numerical schemes, turbulent combustion models and the regular increase of computing power allow Large Eddy Simulation (LES) to be applied to real industrial burners.
Staffelbach, Gabriel +2 more
core +1 more source
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.
doaj +1 more source
Macromolecular Symposia, EarlyView.ABSTRACT This study aims to validate the structural and thermomechanical reliability of an additively manufactured test chamber specifically designed for the experimental investigation of sustainable aviation fuel (SAF) atomization under jet‐in‐crossflow (JICF) conditions representative of gas turbine afterburners. The proposed test chamber is designed
Valerio Acanfora +4 more
wiley +1 more source
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
openaire +1 more source
Soot production in a tubular gas turbine combustor [PDF]
, 1994 Soot production in gas turbine combustors is not desirable since it is the major source of exhaust smoke emission and its thermal radiation to the combustor liner deteriorates the liner durability.
Zheng, Qing-ping, Zeng, Q
core
Experimental investigations into high-altitude relight of a gas turbine
, 2008 This thesis describes experiments to investigate high-altitude relight of a lean direct injection (LDI) combustor. The features that make LDI technology less polluting in terms of NOx compared to conventional combustors are expected to impede relight ...
Read, Robert William
core +1 more source
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
doaj +1 more source
Carbon Neutralization, Volume 5, Issue 4, July 2026.Overview of polymeric and mixed‐matrix membranes for CO₂ separation, highlighting key materials, fabrication techniques, performance challenges, and innovations supporting industrial decarbonization and sustainable development. ABSTRACT Carbon dioxide (CO₂) emissions from anthropogenic sources are major contributors to global warming and climate change,
Muhammad Mansha +5 more
wiley +1 more source
Multi-objective computational engineering design optimisation for micro-combustor devices [PDF]
, 2013 This thesis describes the development of a multi-objective automated optimisation system to be used for the design optimisation of micro-scale combustion devices.
Saddawi, Salwan David
core
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
doaj +1 more source