Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Soot And Radiation In A Gas Turbine Combustor
Download Soot And Radiation In A Gas Turbine Combustor full books in PDF, epub, and Kindle. Read online Soot And Radiation In A Gas Turbine Combustor ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Soot and Radiation in a Gas Turbine Combustor by : A. H. Lefebvre
Download or read book Soot and Radiation in a Gas Turbine Combustor written by A. H. Lefebvre and published by . This book was released on 1987 with total page 135 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of pressure, inlet air temperature, and fuel type on the soot threshold or critical equivalence ratio, are presented. Higher pressures yield lower soot thresholds, while no dependence on fuel type, as described by either the fuel hydrogen-to-carbon ratio, fuel molecular weight, number of carbon atoms, or number of carbon-carbon bonds, is observed. Variations in inlet air temperature have a complex effect; however, the results clearly show that the experimentally measured flame temperature is central to a description of the incipient soot formation process. The critical equivalence ratio dependence on pressure and temperature is shown to agree with a two-step semi-global model for soot precursor evolution for pressures form 0.1 to 0.8 MPa, and measured flame temperatures between 1600 and 2400K. The effects of equivalence ratio, pressure, and fuel chemistry on total non-luminous flame radiation were also studied. Radiant intensity was highest for an equivalence ratio of unity and increased linearly with pressure from 0.4 to 0.8 MPa. Keywords: Incipient soot formation, Flame radiation and emissivity, Premixed flames, Pressure dependence.
Book Synopsis Gas Turbine Combustor Soot and Radiation Studies by : Jim Alan Clark
Download or read book Gas Turbine Combustor Soot and Radiation Studies written by Jim Alan Clark and published by . This book was released on 1981 with total page 368 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Soot and Thermal Radiation in a Model Gas Turbine Combustor Burning Kerosene Fuel Spray at Different Swirl Levels by :
Download or read book Prediction of Soot and Thermal Radiation in a Model Gas Turbine Combustor Burning Kerosene Fuel Spray at Different Swirl Levels written by and published by . This book was released on 2016 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Soot Production in a Tubular Gas Turbine Combustor by :
Download or read book Soot Production in a Tubular Gas Turbine Combustor written by and published by . This book was released on 1901 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: 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. Soot formation involves comparatively slow chemistry and equilibrium can not be applied to soot modelling in the combustor flow field. . The exact sooting process in the combustor is poorly understood given both the complexity and the limited experimental data available. The work reported in this thesis seeks to first develop in-situ techniques for retrieving spatially-resolved soot properties, mainly soot particle volume fraction, from within the combustor and also to apply the measured results to comparisons with predicted soot concentrations. Two probing methods have been demonstrated which also incorporate a laser absorption technique. The sight probe proves to be more reliable in the present measurements. The evaluation of the physical probing techniques in sooty laboratory flames reveals that the flame structure will not be substantially distorted by the probe. The disturbance caused by the probe is localised, a feature which is evident in the reported water flow visualization test. The necessary inert gas purge can be minimised to reduce the local aerodynamic perturbation. The measured soot volume fraction distributions are comparable with sooting levels reported in flame studies in the literature. The peak soot volume fractions are located off-axis, characteristic of the fuel atornization. The measurementsin the primary zone are restricted by the multi-phase character of the flow, where soot absorption can not be readily discriminated from fuel droplet scattering. Measurements are reported over a range of air-fuel ratios, inlet pressures and temperatures. Time-averageds calard istributionsa t the nominald ilution sectionh ave beeno btained in addition to the soot measuremenut sing probe sampling and standard gas analysis. Correlationso f carbond ioxide with mixtur.
Book Synopsis Effects of Broadened Property Fuels on Radiant Heat Flux to Gas Turbine Combustor Liners by :
Download or read book Effects of Broadened Property Fuels on Radiant Heat Flux to Gas Turbine Combustor Liners written by and published by . This book was released on 1983 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Soot and Radiation Modelling in Gas Turbine Combustion Chambers by : H.T. Brocklehurst
Download or read book Soot and Radiation Modelling in Gas Turbine Combustion Chambers written by H.T. Brocklehurst and published by . This book was released on 1997 with total page 221 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flow and Combustion in Advanced Gas Turbine Combustors by : Johannes Janicka
Download or read book Flow and Combustion in Advanced Gas Turbine Combustors written by Johannes Janicka and published by Springer Science & Business Media. This book was released on 2012-10-29 with total page 495 pages. Available in PDF, EPUB and Kindle. Book excerpt: With regard to both the environmental sustainability and operating efficiency demands, modern combustion research has to face two main objectives, the optimization of combustion efficiency and the reduction of pollutants. This book reports on the combustion research activities carried out within the Collaborative Research Center (SFB) 568 “Flow and Combustion in Future Gas Turbine Combustion Chambers” funded by the German Research Foundation (DFG). This aimed at designing a completely integrated modeling and numerical simulation of the occurring very complex, coupled and interacting physico-chemical processes, such as turbulent heat and mass transport, single or multi-phase flows phenomena, chemical reactions/combustion and radiation, able to support the development of advanced gas turbine chamber concepts
Book Synopsis Fuel Molecular Structure and Flame Temperature Effects on Soot Formation in Gas Turbine Combustors by :
Download or read book Fuel Molecular Structure and Flame Temperature Effects on Soot Formation in Gas Turbine Combustors written by and published by . This book was released on 1989 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Correlation of Soot Formation in Turbojet Engines and in Laboratory Flames by : Robert K. Gould
Download or read book Correlation of Soot Formation in Turbojet Engines and in Laboratory Flames written by Robert K. Gould and published by . This book was released on 1981 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: Data obtained from aviation gas turbine combustor tests have been examined to determine the effects of fuel properties on soot-related measurements such as engine smoke number, combustor flame radiation, and/or combustor linear temperature. Some tests of smaller laboratory combustors used to simulate these large combustors were also examined. From the existing data it is clear that soot production is a strong function of the fuel chemical composition. Variations in the physical properties of the fuel do not correlate well with soot-related effects. In studies in which a broad range of fuel properties was examined, correlation of soot-related effects with basic fuel compositional parameters including (1) the hydrogen content of the fuel, (2) the aromatic content of the fuel, and (3) the amount of multiple-ring aromatics in the fuel show that typically only the first of these correlates well. However, it has also been shown that fuel compositions can be chosen for which this correlating parameter fails.
Book Synopsis Fundamentals of Soot Formation in Gas Turbine Combustors by :
Download or read book Fundamentals of Soot Formation in Gas Turbine Combustors written by and published by . This book was released on 1998 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental facility for studying soot formation in high temperature, fuel-rich, laminar, premixed flames has been constructed. Diagnostics included laser absorption, thermocouple particle densitometry, and thermophoretic soot sampling with analysis by transmission electron microscopy. Single particles with diameters as small as 3-5 nanometers were observed. Larger particles (20-25 nanometers) agglomerated to form large clusters. A coflow, axisymmetric, laminar ethylene diffusion flame has been studied, both experimentally and computationally. A lifted flame has been selected to eliminate possible uncertainties caused by the burner lip. A two-dimensional, detailed soot growth model in which the equations for particle production are coupled to the flow and gaseous species conservation equations has been used to investigate soot production in the flame. Detailed transport and finite rate chemistry in the gas phase was coupled with the particle aerosol equations in the sectional representation. In comparison to measured data obtained using intrusive and non- intrusive diagnostics, the model predicted temperature, flame height, and major species very well. Peak benzene concentrations and soot volume fraction were predicted to within 20% of the experimental value. The predicted distribution of benzene was excellent, but the soot was underpredicted along the centerline. This deficit was attributed to limitations in the PAH growth model. Oxidation of particulates was dominated by reactions with hydroxyl radical at superequilibrium levels. Radiation losses significantly effected predicted temperatures.
Book Synopsis GAS Turbine Combustion, Second Edition by : Arthur H. Lefebvre
Download or read book GAS Turbine Combustion, Second Edition written by Arthur H. Lefebvre and published by CRC Press. This book was released on 1998-09-01 with total page 420 pages. Available in PDF, EPUB and Kindle. Book excerpt: This revised edition provides understanding of the basic physical, chemical, and aerodynamic processes associated with gas turbine combustion and their relevance and application to combustor performance and design. It also introduces the many new concepts for ultra-low emissions combustors, and new advances in fuel preparation and liner wall-cooling techniques for their success. It details advanced and practical approaches to combustor design for the clean burning of alternative liquid fuels derived from oil shades, tar sands, and coal. Additional topics include diffusers, combustion performance fuel injection, combustion noise, heat transfer, and emissions.
Book Synopsis Fuel Effects on Gas Turbine Combustors and Engines. An Annotated Bibliography by : COORDINATING RESEARCH COUNCIL INC ATLANTA GA.
Download or read book Fuel Effects on Gas Turbine Combustors and Engines. An Annotated Bibliography written by COORDINATING RESEARCH COUNCIL INC ATLANTA GA. and published by . This book was released on 1981 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt: Partial Contents Include: (1) Flame Radiation, Combustion Liner Temperature, and Combustor Liner Durability; (2) Exhaust Smoke and Soot Formation; (3) Gaseous Emissions and Combustion Efficiency; (4) Flame Ignition and Stability, Reaction Rates, and Spray Characteristics; and (5) Carbon Deposition.
Book Synopsis Gas Turbine Emissions by : Timothy C. Lieuwen
Download or read book Gas Turbine Emissions written by Timothy C. Lieuwen and published by Cambridge University Press. This book was released on 2013-07-08 with total page 385 pages. Available in PDF, EPUB and Kindle. Book excerpt: The development of clean, sustainable energy systems is a preeminent issue in our time. Gas turbines will continue to be important combustion-based energy conversion devices for many decades to come, used for aircraft propulsion, ground-based power generation, and mechanical-drive applications. This book compiles the key scientific and technological knowledge associated with gas turbine emissions into a single authoritative source.
Book Synopsis Gas Turbine Combustor Design Problems by : Arthur Henry Lefebvre
Download or read book Gas Turbine Combustor Design Problems written by Arthur Henry Lefebvre and published by Hemisphere Pub. This book was released on 1980 with total page 458 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781725612235 Total Pages :34 pages Book Rating :4.6/5 (122 download)
Book Synopsis Effects of Broadened Property Fuels on Radiant Heat Flux to Gas Turbine Combustor Liners by : National Aeronautics and Space Administration (NASA)
Download or read book Effects of Broadened Property Fuels on Radiant Heat Flux to Gas Turbine Combustor Liners written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-14 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of fuel type, inlet air pressure, inlet air temperature, and fuel/air ratio on the combustor radiation were investigated. Combustor liner radiant heat flux measurements were made in the spectral region between 0.14 and 6.5 microns at three locations in a modified commercial aviation can combustor. Two fuels, Jet A and a heavier distillate research fuel called ERBS were used. The use of ERBS fuel as opposed to Jet A under similar operating conditions resulted in increased radiation to the combustor liner and hence increased backside liner temperature. This increased radiation resulted in liner temperature increases always less than 73 C. The increased radiation is shown by way of calculations to be the result of increased soot concentrations in the combustor. The increased liner temperatures indicated can substantially affect engine maintenance costs by reducing combustor liner life up to 1/3 because of the rapid decay in liner material properties when operated beyond their design conditions. Haggard, J. B., Jr. Glenn Research Center NASA-TM-83537, E-1906, NAS 1.15:83537 RTOP 505-31-42...
Book Synopsis Oxygen-Enhanced Combustion by : Charles E. Baukal Jr.
Download or read book Oxygen-Enhanced Combustion written by Charles E. Baukal Jr. and published by CRC Press. This book was released on 2013-03-15 with total page 779 pages. Available in PDF, EPUB and Kindle. Book excerpt: Combustion technology has traditionally been dominated by air/fuel combustion. However, two developments have increased the significance of oxygen-enhanced combustion-new technologies that produce oxygen less expensively and the increased importance of environmental regulations. Advantages of oxygen-enhanced combustion include less pollutant emissi
Book Synopsis High Pressure Combustor Flame and Wall Conjugate Radiative Heat Transfer by : Andressa Johnson
Download or read book High Pressure Combustor Flame and Wall Conjugate Radiative Heat Transfer written by Andressa Johnson and published by . This book was released on 2020 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Efficient aeronautical engines operate at higher pressure ratios and temperature, creating challenges due to higher heat loads. Thermal radiation in aviation has conventionally been treated as correction factors or scaled from experimental data. The complexity of the radiative transfer equation (RTE) leads to computational costly solutions resulting in simplified treatment. The goal of this work is to extend knowledge of non-gray gas radiation modeling to gas-turbine combustor simulations under high-pressure conditions. A one-dimensional temperature solver for combustor liners with thermal barrier coating is developed first, and a non-gray wide-band spectral model for high-pressure conditions is constructed subsequently. Both retrieve spectral properties of combustion gases from high-resolution spectroscopy databases and a Monte Carlo ray tracing solver is used to provide accurate solution of RTE in the gas phase. Frozen-field analysis of a model gas turbine combustor shows heat fluxes concentrated downstream of the main flame brush. Increase of pressure from 1 bar to 40 bar enhances peak radiation loads to the wall by approximately ten folds. A wide-band model is subsequently proposed for gas and soot under pressurized conditions. Improvement in radiative flux prediction is observed when the band definition is carefully chosen around radiative emission peaks, although overall the wide-band model approximates the gray solutions obtained using the MCRT solver closely. Further research is needed to better characterize liner temperature by considering more realistic radiative and convective heat load and TBC parameters. Improvement of the wide-band model is required to better predict the non-gray radiative heat load to the wall.
