Relevant bibliographies by topics / Nozzle for air-placed co

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  1. Journal articles
  2. Dissertations / Theses
  3. Book chapters
  4. Conference papers

Academic literature on the topic 'Nozzle for air-placed co'

Author: Grafiati
Published: 4 June 2021
Last updated: 4 February 2022

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Journal articles on the topic "Nozzle for air-placed co"

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Papanikolaou, N., and I. Wierzba. "Effect of Burner Geometry on the Blowout Limits of Jet Diffusion Flames in a Co-Flowing Oxidizing Stream." Journal of Energy Resources Technology 118, no. 2 (June 1, 1996): 134–39. http://dx.doi.org/10.1115/1.2792704.

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The effects of changes in the jet nozzle geometry, i.e., nozzle shape and lip thickness, on the blowout limits of jet diffusion flames in a co-flowing air stream were experimentally investigated for a range of co-flow air stream velocities. Circular and elongated nozzles of different axes rations were employed. Preliminary results showed that nozzles with low major-to-minor axes ratios improved, while high ratios reduced, the blowout limit of attached flames compared with that for an equivalent circular nozzle. The nozzle shape had no apparent influence on the blowout limits lifted flames and the limiting stream velocity. The experimental blowout limits of lifted flames were found to be a function of the co-flowing stream velocity and jet discharge area. On the other hand, the stability of attached flames was a function of the co-flowing stream velocity, jet discharge area as well as the nozzle shape. The effect of premixing a fuel with the surrounding air was also studied. Generally, the introduction of auxiliary fuel into the surrounding stream either increased or decreased the blowout limit depending on the type of flame stabilization mechanism prior to blowout. The stability mechanism of the flame was found to be a function of the co-flow stream velocity and the auxiliary fuel employed.
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Papanikolaou, N., and I. Wierzba. "The Effects of Burner Geometry and Fuel Composition on the Stability of a Jet Diffusion Flame." Journal of Energy Resources Technology 119, no. 4 (December 1, 1997): 265–70. http://dx.doi.org/10.1115/1.2795000.

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The effect of the burner configuration and fuel composition on the stability limits of jet diffusion flames issuing into a co-flowing air stream is presented. Circular and elliptic nozzles of various lip thicknesses and aspect ratios were employed with methane as the primary fuel and hydrogen, carbon dioxide, and nitrogen as additives. It was found that the effects of nozzle geometry, fuel composition, and co-flowing stream velocity on the blowout limits were highly dependent on the type of flame stabilization mechanism, i.e., whether lifted or rim-attached, just prior to blowout. The blowout behavior of lifted flames did not appear to be significantly affected by a change in the nozzle shape as long as the discharge area remained constant, but it was greatly affected by the fuel composition. In contrast, attached flame stability was influenced by both the fuel composition and the nozzle geometry which had the potential to extend the maximum co-flowing stream velocity without causing the flame to blow out. The parameters affecting the limiting stream velocity were studied.
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Kirsanov, Yu A., D. V. Makarushkin, and A. Yu Kirsanov. "INFLUENCE OF THE SWITCHING PERIODS FREQUENCY ON THE THERMAL EMISSIVITY OF A REGENERATIVE AIR PREHEATER." Proceedings of the higher educational institutions. ENERGY SECTOR PROBLEMS 20, no. 7-8 (September 8, 2018): 35–46. http://dx.doi.org/10.30724/1998-9903-2018-20-7-8-35-46.

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A laboratory stand with a regenerative air preheater, an automated control system and measurement of airflow parameters and a nozzle designed to study the heat transfer of a packet of parallel plates under non-stationary conditions for different periods is described. The technique of measuring the unsteady temperature of cold and hot coolant flows adjusted for inertia of the thermocouples and the method of measuring the heat transfer co efficient of plates. The time variations of the Nusselt number and the heat load transmitted by the nozzle for individual periods are shown. Obtained in experiments with the packages of plates of different materials and thickness values of the average Nusselt number for the period criterial generalized equation for convenient engineering calculations RAPH with leaf nozzles of various types.
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Lee, Cheolwoo, Insu Kim, and Junggoo Hong. "Experimental Investigation of Air–Fuel Mixing Effects on Flame Characteristics in a Direct fired Burner." Energies 14, no. 12 (June 15, 2021): 3552. http://dx.doi.org/10.3390/en14123552.

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The length and pattern of air–fuel mixing plays a significant role in the uniformity, flame temperature, and emission characteristics, which can lead to a superior product quality in a non-oxidizing direct fired burner for a cold-rolled steel plate furnace. In this study, a diffusion-flame-type burner and partially-premixed-type burner were experimentally investigated to understand their effects on flame shape, flame temperature, and exhaust gas characteristics. With this aim, fuel nozzle size, nozzle hole number, fuel injection angle, and mixing distance of fuel and air were varied during the experiments. Computational fluid dynamics simulations were also performed to investigate the air–fuel mixing state for a nozzle-mixed burner and a partially-premixed burner. The results show that the flame temperature of the partially-premixed burner increases by up to 26 °C on average compared to that of the nozzle-mixed burner. It is also shown that the mixing distance plays an important role in the flame temperature of the partially-premixed burner. In addition, the residual oxygen concentration and volume ratio of CO/CO2 in the flue gas of the partially-premixed burner exhibit lower concentrations compared to those of the diffusion flame burner.
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Lambosi, Latip, Amir Khalid, Bukhari Manshoor, Shahrin Hisyam, and Lo Kok Hao. "Effect of Nozzle Angle to Combustion Characteristic in Biodiesel Burner." Applied Mechanics and Materials 773-774 (July 2015): 585–89. http://dx.doi.org/10.4028/www.scientific.net/amm.773-774.585.

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The increasing effort on the environmental impacts of fossil fuel based power generation has led to increased research with the aim of reducing emissions and improving combustion efficiency by turning to alternative fuel such as biodiesel. But the hazardous emission caused by biodiesel is still a problem that need to tackle. One of way to achieve this is by choosing the correct nozzle characteristic. In the current study, the effect of nozzle angle on mixture formation and combustion characteristic are investigate using air-assisted fuel atomizing biodiesel burner. The nozzle angle that was used are θ = 450 and 500. The results show with nozzle 450 produce lower spray penetration, but higher spray angle and spray area compare to nozzle 500. The result are similar on flame development. For the emission characteristic, the Carbon Monoxide (CO) and Hydro Carbon (HC) emission had a strong reduction by using nozzle with 450 angle compare to 500 angle.
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Ghaem-Maghami, E., and H. Johari. "Concentration Field Measurements Within Isolated Turbulent Puffs." Journal of Fluids Engineering 129, no. 2 (July 6, 2006): 194–99. http://dx.doi.org/10.1115/1.2409348.

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The structure of passive scalar concentration field within isolated turbulent puffs was measured using the planar laser Mie scattering technique. Puffs were generated by injecting seeded air through a 5-mm-diameter nozzle into a chamber with a weak air co-flow. The injection time and volume was varied by the use of a fast-response solenoid valve. Puffs were examined in the range of 25–55 diameters downstream of the nozzle. The Reynolds number based on the average velocity and nozzle diameter was 5000. The results indicate that as the injection volume increases, puffs evolve from a spherical geometry to that with a tail. The half-width of radial concentration profiles through the puff center decrease as the injection volume increases. On the other hand, the puff length in the axial direction increases with the injection volume. The volume of ambient fluid entrained by the puff, and normalized by the injected volume, decreases with increasing injection volume.
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Rao, A. K., C. H. Melcher, R. P. Wilson, E. N. Balles, F. S. Schaub, and J. A. Kimberley. "Operating Results of the Cooper-Bessemer JS-1 Engine on Coal–Water Slurry." Journal of Engineering for Gas Turbines and Power 110, no. 3 (July 1, 1988): 431–36. http://dx.doi.org/10.1115/1.3240139.

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Successful operation of the Cooper-Bessemer JS-1 engine on coal–water slurry (CWS) fuel has been achieved at full power output, part load, and part speed conditions with varying degrees of diesel pilot fuel including zero pilot (auto-ignition of CWS). Selected results of the effect of pilot fuel quantity, pilot fuel timing, and manifold air temperature on engine performance are presented. Also, the influence of injector nozzle hole size and CWS mean particle size on engine performance is studied. High injection pressures resulted in good atomization of CWS and in combination with heated combustion air resulted in short ignition delays and very acceptable fuel consumption. Low CO/CO2 ratios in exhaust gas analysis confirmed good combustion efficiency. NOx emissions are compared for CWS and diesel fuel operation of the engine. Effect of injector nozzle hole size and manifold air temperature on NOx emissions is studied.
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Madanahalli, A. V., and S. R. Gollahalli. "Effects of Nozzle Orientation on the Structure and Emissions of Spray Flames." Journal of Energy Resources Technology 115, no. 3 (September 1, 1993): 183–89. http://dx.doi.org/10.1115/1.2905991.

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An experimental study of the effects of the orientation of the liquid fuel stream relative to the air stream from a twin fluid atomizer located in an open-jet wind tunnel is presented. The orientation angle was set at 0 (concurrent), 45, 90, 135, and 180 deg (directly opposed). At 45 and 90 deg, the flame length, the radiation emission, and the concentrations of carbon monoxide, carbon dioxide, nitric oxide, and soot are higher than those at co-flow conditions. At 135 deg, all these quantities decrease markedly from their values at 90 deg and again increase when the fuel and air streams are directly opposed (180 deg). These changes are discussed in terms of the influx of air and recirculation of combustion products into the salient zones of the flame.
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Stapper, B. E., W. A. Sowa, and G. S. Samuelsen. "An Experimental Study of the Effects of Liquid Properties on the Breakup of a Two-Dimensional Liquid Sheet." Journal of Engineering for Gas Turbines and Power 114, no. 1 (January 1, 1992): 39–45. http://dx.doi.org/10.1115/1.2906305.

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The breakup of a liquid sheet is of fundamental interest in the atomization of liquid fuels. The present study explores the breakup of a two-dimensional liquid sheet in the presence of co-flow air with emphasis on the extent to which liquid properties affect breakup. Three liquids, selected with varying values of viscosity and surface tension, are introduced through a twin-fluid, two-dimensional nozzle. A pulsed laser imaging system is used to determine the sheet structure at breakup, the distance and time to breakup, and the character of the ligaments and droplets formed. Experiments are conducted at two liquid flow rates with five flow rates of co-flowing air. Liquid properties affect the residence time required to initiate sheet breakup, and alter the time and length scales in the breakup mechanism.
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Uchiyama, Tomomi, and Akihito Fukase. "Three-Dimensional Vortex Method for Gas-Particle Two-Phase Compound Round Jet." Journal of Fluids Engineering 127, no. 1 (January 1, 2005): 32–40. http://dx.doi.org/10.1115/1.1852490.

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This paper proposes a three-dimensional vortex method for a gas-particle two-phase compound round jet. The method can take account of the interaction between the two phases by calculating the motion of particles and the behavior of gas vortex elements through the Lagrangian approach. In order to discuss the validity of the method, an air jet, loaded with small glass particles, issuing from a round nozzle into the co-flowing air stream is simulated. The simulation demonstrates that the air turbulence modulations due to the particles, such as the relaxation of velocity decay, the decrement of momentum diffusion in the radial direction at the fully developed region, and the reduction of turbulent intensity and Reynolds shear stress, are successfully captured by the method.
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Dissertations / Theses on the topic "Nozzle for air-placed co"

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Schach, Rainer, and Manuel Hentschel. "Grundlagen für die Nutzwertanalyse für Verstärkungen aus textilbewehrtem Beton." Saechsische Landesbibliothek- Staats- und Universitaetsbibliothek Dresden, 2009. http://nbn-resolving.de/urn:nbn:de:bsz:14-ds-1244049476991-75979.

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Im Rahmen des Transferprojektes sollen baubetriebliche Rahmenbedingungen und Kennwerte, die zur Beurteilung der wirtschaftlichen Anwendung des Verfahrens geeignet sind, erarbeitet werden. Untersucht werden soll die Applikation von textilbewehrtem Beton im Bereich der Sanierung und Verstärkung von großflächigen Betonbauteilen. Generell können Bauaufgaben in sehr vielen Fällen durch verschiedene Bauverfahren realisiert werden, die sich regelmäßig hinsichtlich der Kosten, der benötigten Bauzeit aber auch hinsichtlich der gelieferten Qualität und des Einflusses auf die Umwelt unterscheiden. Aus baubetrieblicher Sicht wird traditionell über den kalkulatorischen Verfahrensvergleich jenes Verfahren ermittelt, mit dem die Realisierung am wirtschaftlichsten ausgeführt werden kann. Falls qualitative Kriterien beim Verfahrensvergleich mit berücksichtigt werden sollen, stehen verschiedene Methoden zur Auswahl. Der Begriff Nutzwertanalyse wird häufig als Synonym für diese nichtmonetären Bewertungsverfahren verwendet. In diesem Sinne ist auch der Titel des Beitrages zu verstehen. Die Grundlage bilden die baubetrieblichen Rahmenbedingungen, welche im Rahmen dieses Forschungsprojektes bestimmt werden. Hierzu zählen unter anderem die Entwicklung einer Trockenmischung des zu verwendenden Betons aus der bisher verwendeten Standardrezeptur der TU Dresden und geeigneter Maschinen für die Applikation des textilbewehrten Betons.
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Book chapters on the topic "Nozzle for air-placed co"

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Balasubramanian, Prabakaran. "An Attempt in Blending Higher Volume of Ethanol with Diesel for Replacing the Neat Diesel to Fuel Compression Ignition Engines." In Bioethanol [Working Title]. IntechOpen, 2020. http://dx.doi.org/10.5772/intechopen.95263.

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Alcohols are renewable in nature and can be manufactured from biomass. Butanol a higher alcohol, can be utilized as co-solvent to prevent the phase separation of diesel-ethanol blends as per the previous researches.. This experimentation has been conducted with the blends of diesel-ethanol with various proportions of n-butanol followed by the solubility test in the temperature range of 5–25°C. The results indicate that 45% of ethanol can be blended with diesel by the assistance of 10% of n-butanol to make the final blend stable up to a temperature of 5°C for 20 days, which met the requirements of the essential properties (ASTM). Existing diesel engine has been modified as per the optimal level of parameters such as intake air temperature (IAT), fuel injection timing (FIT), nozzle opening pressure (NOP) and compression ratio (CR) obtained using Taghuchi method of L9 orthogonal array. Arrived out parameters are 75°C of IAT, 29°before top dead centre of FIT, 210 bar of NOP and 19: 1 of compression ratio. The implementation of these parameters in diesel engine and fueling with diesel-ethanol butanol blend containing 45% ethanol produced closer performance and emissions characteristics compared to that of diesel. However, the emissions of smoke, hydrocarbon and carbon monoxide produced by the optimal blend are found to be marginally higher compared to that of diesel. These can be ratified by the introduction of after treatment systems modifications.
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Balasubramanian, Prabakaran. "An Attempt in Blending Higher Volume of Ethanol with Diesel for Replacing the Neat Diesel to Fuel Compression Ignition Engines." In Bioethanol Technologies. IntechOpen, 2021. http://dx.doi.org/10.5772/intechopen.95263.

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Alcohols are renewable in nature and can be manufactured from biomass. Butanol a higher alcohol, can be utilized as co-solvent to prevent the phase separation of diesel-ethanol blends as per the previous researches. This experimentation has been conducted with the blends of diesel-ethanol with various proportions of n-butanol followed by the solubility test in the temperature range of 5–25°C. The results indicate that 45% of ethanol can be blended with diesel by the assistance of 10% of n-butanol to make the final blend stable up to a temperature of 5°C for 20 days, which met the requirements of the essential properties (ASTM). Existing diesel engine has been modified as per the optimal level of parameters such as intake air temperature (IAT), fuel injection timing (FIT), nozzle opening pressure (NOP) and compression ratio (CR) obtained using Taghuchi method of L9 orthogonal array. Arrived out parameters are 75°C of IAT, 29° before top dead centre of FIT, 210 bar of NOP and 19: 1 of compression ratio. The implementation of these parameters in diesel engine and fueling with diesel-ethanol butanol blend containing 45% ethanol produced closer performance and emissions characteristics compared to that of diesel. However, the emissions of smoke, hydrocarbon and carbon monoxide produced by the optimal blend are found to be marginally higher compared to that of diesel. These can be ratified by the introduction of after treatment systems modifications.
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"ahcutm io annslairfee , m pr oosptee rt f y fe , c a ti nvdep if roddo uctive capacity. These is a critical element of the hydrological system. fervoem nt . o T ne hena ty tu preaslohrafzoarrmdstoofam no it n ig eaitn io nadavcat nce of the Information on the status of snowpack conditions can m ther. Droug iv hitt -i reeslavtaerdyfporroevciadsets co onfsb id e e lo ra w b -le noardmvaalncse tr dealm ea f d lo t w im aend fo rrerseelr ia vbolierf th ro it m ig ati e in tshioosne act diou u s se io dnfsoraroet , h e for the most part, different levels. gation is the indaetnutrie fi coaf ti ohran za artd ural hazards because of •Monitoring and early warning refers to activities with previous droughts a n of t . heAifm ir psatcsttsepa ss in ocm iat i e ti d ­ tdheacti si pornovm id aekeirnsfo at r m al a l ti l o ev neltsho at ftchaenobneseutsoefddtroouaglhetr . t w th ietshefium tu praectds ro (a ungdhtotehvee rs n ) daarnea li skseelsysm to enbteoafsw so hcei ther This information can be used by planners, emergency actions can be identifie n d ts. From this point, spec aitfeidcimmapnlaegmee rs n , tpporlo ic g y ra amnmdedsecainsd io pnom lic aikees rs th , aatnwd il o l th he elrpsttooo fu f t ur im epdarcotus gh atsseovceinattse . d Pa rttoIV re edm uc pehatsh is eesim th peacr ts of reduce the risk associated with the hazard. Moni­ geographical settings as wwie th ll adsrom ug et hhtodionl og viaerasinoguest to doa ri cat tia ng activities include the collection and analysis of quantify these impacts. Part V considers adjustment user o , ndo at fadaptraodpu ro cdtudcetvsetloopdm ec einsti , onanmdak th e e rs caonmdm ot uhneir ­ a an nddaPdaarpt ta V ti Ioncosn tr caetn eg tr iaetsesemopnlopyreedpatroed re ndeu ss cem im et phaocd ts ­ h in aza s r . dDsabtuat in a cludes not only physical data related to olo the definit lisoon so ocfiavlualn ne drabb io il lio ty g . icA al d co a m ta ptrheahtenassisv is ethgaavtg io ie n s , pr iong st ria tu m ti m on es alaanrdr an a g ct eim on esn , ts a /c nadpapco it liiecs ie , s miti­ drought monitoring system would include the collec­ imp e a ct bseo en f dr oorugchotu . ld be employed to reduce th th aetp ti roenc ip o it f a tio cl n i ) maastow lo el gliacsals tre daam ta f lo ( w e. , g r . e , se trevm oi prearnad tu grreouanndd ­ t • oPrienpcarreeadsneestshe re fleervseltoofprreedaidsiansetsesraocr tivities designed w se a n ter levels, soil moisture, snowpack, and remo improve oper­ cast ssedodfataagfrriocm satellites. This information is useful in ftoerley ­ aan ti on eamlearngdenicnys tit ( uet . igo ., naelacra ly p ab w il air ti neisng fo rsryess te p m on s, d in ogpetro ­ itnod ri i n ce gsatnodte ra acru ly ltw ur aarlnianngdtehcyhdnrioqluoegsi , cianlcldurdoiungghtth . e M us oeno i­ f u at sieofnuallfpolrands) e . no Fto in rgdrpor ught, contingency plans are them in a histo kriccu al rrent d ogrammatic responsibilities; contex ro t, u is g h th teco su nbdjie ti cotnosfaPnadrttIoIIv . iew p im ol p ic rioevsinbgetiw nf eoernmaatn io dnw fl iotw hi nonlesveev ls e ri o ty, im and coordination between levels of gov fergnomv pac eenrtn ts m , ean nd . t; d •P ec re is diiocn ti / opnolriecfyermsatkoerascw tiv it it hieasdtvhaantcepd ro fvoirdeecauss ts eros and D f the m sh a ro l ught i oul pdarntoosfan th i e nsidi t be vi ecw li e m ou aste nat d as m of ural hazard tha erveilrytuaalp ly hyaslilcarletg is pihoaensn no . omIrt ­ o ­ a fo crcm ur s r , ebnu ce tporfodbraobu il g it hyt . These forecasts can take many enon. Rather, drought is the result of an interplay p n re ddi in ct tieonnss it . yoFrorseecvaes ri ttyo ) fiso ccurrenc accu ursaucay ll yiaes so (t c im iat e e , ddw ura s highly viatrh ti o th n e , w be attw er eesnua natural event and the demand placed on between natural iable be consi pdpelryedbyrh el uam tiv aen -u to se ssoym ste emlso . nDg-rtoeurgmhtasvheo ra u g ld eidm ro puogrh ta ts ntincom ns oishtapzaarrtdssoafntdhe is w pa orrtlidc . ulLae rl deration for drought fore aydltiimm it eed is f a or condition of balance between precipitation and so d casts as well n , eva M po atnry an dsepfiirnaittiioonn . s of drought exist; it is unrealistic a in ncdorepco is riaotnem th akers are given ample opportunity to to expect a universal definition to be derived. Th the imple imseinntfao ti romnato io fnmiin ti g p at liaonnn in pr gogsrta ra m te mge ie s s . sDpreocu ti g ve htc as anfboe ll ogw ro s: u pe mdetbeyortoylpoegiocfald , isc hiypd li rnoalroygipcearl ­ , c lo agse ts reof is m al estoeoarno lo im gi pcoarl ta d n ro tudg is httinacn ti don th boe se tw oefenhyfdorroe -­ ian gric ical drought, especially in regions where snowpack so cco io rup ltur ec o o ra ntaels , d an omic if d f fe re snotc ioeco actors ipnhy it s n ic oaml, ic b . s defini io E lo agcihc al, d is a cipline tion. It mu nsdt /o be r." In Droughts, 46. Routledge, 2016. http://dx.doi.org/10.4324/9781315830896-33.

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Conference papers on the topic "Nozzle for air-placed co"

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Bhargava, Anuj, Donald W. Kendrick, Meredith B. Colket, William A. Sowa, Kent H. Casleton, and Daniel J. Maloney. "Pressure Effect on NOx and CO Emissions in Industrial Gas Turbines." In ASME Turbo Expo 2000: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/2000-gt-0097.

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In order to determine the effect of pressure on emissions and stability limit, an experimental and modeling study has been performed jointly by UTRC and DOE-FETC. Experiments have been performed at lean conditions in 100–400 psi range with two different nozzles. Measured NOx and CO concentrations have been modeled with a PSR Network using detailed chemistry. Good agreement between the data and model predictions over a wide range of conditions indicate the consistency and reliability of the measured data and validity of the modeling approach. Experiments were conducted at the DOE-FETC facility in Morgantown. A simple refractory combustor liner with a fuel-air-premixing nozzle was used to map stability margins, emission levels of NOx, CO and combustion efficiency. Each experimental nozzle had a centerbody and wall pilot for flame stabilization. Data was collected at four different pressures of 100, 200, 300 and 400 psi, and at different diffusion pilot and moisture levels. The premixing nozzle hardware could be easily lit and operated over a broad range of flame temperatures with minimal combustion generated noise. Two different nozzles designed at UTRC were used to determine pressure and nozzle effects. Computations were made for comparison with the experiments. GRI Mech 2.11 kinetics and thermodynamic database was used for modeling the flame chemistry. A Perfectly Stirred Reactor (PSR) network code developed internally at UTRC was used to create a network of PSRs to simulate the flame and combustor. A total of 10 to 15 reactors were used in the network. Residence time varied with the flow rates (air was fixed while fuel flow rate was varied in order to obtain the required equivalence ratio, ϕ). Good agreement between the measured and modeled NOx (5–10%) was obtained, but the agreement for CO (model predictions are higher by 30–50%) was not as good as for NOx. The experimental data and the modeling predictions indicate that the NOx emission functionality with pressure is dependent on both equivalence ratio and absolute pressure. The CO levels tend to go down with increase in pressure as P−0.5, at different equivalence ratios, consistent with an equilibrium analysis.
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Yamamoto, Takeshi, Kazuo Shimodaira, Yoji Kurosawa, Kazuaki Mastuura, Jun Iino, and Seiji Yoshida. "Research and Development of Staging Fuel Nozzle for Aeroengine." In ASME Turbo Expo 2009: Power for Land, Sea, and Air. ASMEDC, 2009. http://dx.doi.org/10.1115/gt2009-59852.

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Research and development of combustion technologies to reduce NOx emission of aero-engines to 20% of ICAO CAEP4 is progressing as a part of a project of JAXA (Japan Aerospace Exploration Agency), the Technology Development for Clean Engine (TechCLEAN). To realize such low NOx level on aero-engines, it is necessary to use not conventional combustion system such as rich-lean combustion but advanced one such as premixed combustion. We are conducting research and development of staging fuel nozzles that use diffusion combustion for the pilot nozzle and premixed combustion for the main nozzle. As the first step, five fuel nozzles were tested experimentally in the form of single-sector combustor. Test conditions were selected as the LTO cycle of presumed small-class engines. From the result of tests, to combine the combustion efficiency in low engine power condition and low NOx emission in high power one, fuel nozzle models that have triple contrary swirler are suitable. However, the combustion efficiency in 7%MTO is lower than that of current engines. It is necessary to decrease the emission of CO.
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Bonnafous, Samuel, Victor Piffaut, Wai-Ho Choy, and Dimitris E. Nikitopoulos. "Local, Near-Field Mixing Augmentation Using Square Coaxial Jets." In ASME Turbo Expo 2004: Power for Land, Sea, and Air. ASMEDC, 2004. http://dx.doi.org/10.1115/gt2004-53985.

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Results from un-forced experiments in flows ensuing from circular and equivalent square coaxial nozzles with parallel sides are presented in this paper. The nozzles are contoured and are designed so that the hydraulic diameters of the internal flow passages are identical for both geometries. The flow experiments were conducted at a co-flow-jet Reynolds number of Re = 16,000 and inner-to-outer jet nominal velocity ratios of λ = 0, 0.5, 1.5. Axis switching, a phenomenon readily observed in single non-axisymmetric nozzles, is shown for the first time to occur in the square coaxial nozzles as well. Comparisons of the mixing regions of the flows from both geometries are made to examine mixing advantages when using square nozzle configurations. Comparisons of stream wise mean velocity fields measured on a center plane parallel to the square nozzle sides, on a diagonal plane of the square nozzle and the center plane of the corresponding circular nozzle, are presented and discussed. Axis switching is shown to be evident in the near-field shear regions for all velocity ratios, resulting in considerable mixing advantages. The spreading rates (and therefore mixing rates) of the outer mixing region of the square nozzles clearly exceed the spreading rate observed in the circular case on the central plane. Axis switching and improved mixing is also observed in the inner mixing region of the square nozzle. This work is relevant to coaxial nozzles for gas turbine combustor applications, although the study has been carried out in a scaled up geometry with respect to this application.
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Saghafi, Fariborz, and Afshin Banazadeh. "Coanda Surface Geometry Optimization for Multi-Directional Co-Flow Fluidic Thrust Vectoring." In ASME Turbo Expo 2009: Power for Land, Sea, and Air. ASMEDC, 2009. http://dx.doi.org/10.1115/gt2009-59715.

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The performance of Co-flow fluidic thrust vectoring is a function of secondary flow characteristics and the fluidic nozzle geometry. In terms of nozzle geometry, wall shape and the secondary slot aspect ratio are the main parameters that control the vector angle. The present study aims to find a high quality wall shape to achieve the best thrust vectoring performance, which is characterized by the maximum thrust deflection angle with respect to the injected secondary air. A 3D computational fluid dynamics (CFD) model is employed to investigate the flow characteristics in thrust vectoring system. This model is validated using experimental data collected from the deflection of exhaust gases of a small jet-engine integrated with a multi-directional fluidic nozzle. The nozzle geometry is defined by the collar radius and its cutoff angle. In order to find the best value of these two parameters, Quasi-Newton optimization method is utilized for a constant relative jet momentum rate, a constant secondary slot height and insignificant step size. In this method, the performance index is described as a function of thrust deflection angle. Optimization parameters (wall geometric parameters) are estimated in the direction of gradient, with an appropriate step length, in every iteration process. A good guess of initial optimization parameters could lead to a rapid convergence towards an optimal geometry and hence maximum thrust deflection angle. Examination over a range of geometric parameters around the optimum point reveals that this method promises the best performance of the system and has potential to be employed for all the other affective factors.
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5

Klein, Sikke, Ivar Austrem, and Jan Mowill. "The Development of an Ultra Low Emissions Liquid Fuel Combustor for the OPRA OP16 Gas Turbine." In ASME Turbo Expo 2002: Power for Land, Sea, and Air. ASMEDC, 2002. http://dx.doi.org/10.1115/gt2002-30107.

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During the last few years OPRA has been working intensively on the development of an ultra low emissions combustor for the OP16 gas turbine. The main focus has been on the combustion of liquid fuels (diesel fuel #2), but a natural gas and a dual fuel system has also been developed. The most important aspect of the development has been the patented Controlled Fuel Air Ratio (COFAR) system incorporating the venturi premixer, the air valve and the fuel injection nozzle. The original diesel fuel injection nozzle of the OP16 was a hybrid design, comprising a pressure swirl central injector surrounded by a classic air-blast atomizer. While the emissions with this fuel nozzle were quite good (30 ppm up to 85% load), subsequent natural gas tests demonstrating single digit emissions, while running at a higher average flame temperature indicated that there was scope for improvement of the fuel preparation system. It was clear that atomization, evaporation and mixing of the diesel fuel could be further improved. For better understanding of the combustion of diesel fuel, an atomization and mixing model was developed, to study the quality of the fuel/air mixture leaving the pre-mixer. Based on the results of this study, a fuel nozzle system, using multipoint injection with small pressure swirl nozzles was selected. Three different sets of atomizers have been evaluated and a nozzle arrangement comprising five identical pressure swirl nozzles showed the best results. The emissions on diesel fuel with the new injector proved very satisfactory. The NOx concentration was kept below 25 ppm from 50% load up to 90% load and below 30 ppm at full load. CO and UHC were well below 10 ppm. These low emissions were achieved by running at a low flame temperature (below 1820K). Furthermore, no combustion dynamics or flame instability was observed.
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6

Merkle, Klaus, Horst Bu¨chner, Nikolaos Zarzalis, and Osman N. Sara. "Influence of Co and Counter Swirl on Lean Stability Limits of an Airblast Nozzle." In ASME Turbo Expo 2003, collocated with the 2003 International Joint Power Generation Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/gt2003-38004.

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This paper presents the reacting flow field and the temperature distribution of two different airblast nozzles, namely co and counter swirl. To support the interpretation of the obtained results, previous measurements of the isothermal flow and mixture field of methane and combustion air are summarized. Velocities within the turbulent flow field were measured by using 3D-LDA, measurements of the field distribution of temperature were performed by means of thermocouple probes. The results show that the counter swirl arrangement provides formation of an additional vortex in the immediate vicinity of the nozzle, which has been observed as well within the isothermal as within the reacting flow. Furthermore, a dampening effect of the tangential velocity profiles towards turbulent exchange of momentum has been observed within the counter swirl configuration. Both effects cause preferential mixing of the fuel with the inner combustion air flow, thereby performing higher concentrations of methane in the near nozzle mixture field. As a consequence the counter swirl flow field exhibits larger areas of near-stoichiometric composition of fuel and air, resulting in an elevated temperature level within the stabilization zone at otherwise identical operation conditions. Therefore, application of a counter swirl nozzle allows a higher thermal load than the co swirl configuration, which offers a satisfying explanation for the wider operating range of the counter swirl burner.
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7

Papanikolaou, N., and I. Wierzba. "The Effect of Co-Flowing Stream Velocities on the Flow Characteristics of Jets Issuing From Elliptic Nozzles." In ASME 1997 Turbo Asia Conference. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/97-aa-074.

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The flow structure of cold and ignited jets issuing into a co-flowing air stream was experimentally studied using a laser Doppler velocimeter. Methane was employed as the jet fluid discharging from circular and elliptic nozzles with aspect ratios varying from 1.29 to 1.60. The diameter of the circular nozzle was 4.6 mm and the elliptic nozzles had approximately the same exit area as that of the circular nozzle. These non-circular nozzles were employed in order to increase the stability of attached jet diffusion flames. The time-averaged velocity and r.m.s. value of the velocity fluctuation in the streamwise and transverse directions were measured over the range of co-flowing stream velocities corresponding to different modes of flame blowout that are identified as either lifted or attached flames. On the basis of these measurements, attempts were made to explain the existence of an apparent optimum aspect ratio for the blowout of attached flames observed at higher values of co-flowing stream velocities. The insensitivity of the blowout limits of lifted flames to nozzle geometry observed in our previous work at low co-flowing stream velocities was also explained.
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8

Zhang, Luzeng, Juan Yin, and Hee Koo Moon. "The Effect of Compound Angle on Nozzle Pressure Side Film Cooling." In ASME Turbo Expo 2009: Power for Land, Sea, and Air. ASMEDC, 2009. http://dx.doi.org/10.1115/gt2009-59141.

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The effect of film cooling hole compound angle on nozzle pressure side film cooling effectiveness was experimentally investigated using a single row of shaped hole injection. The engine operating conditions were simulated in a scaled warm cascade, which was built based on industrial gas turbine nozzle vanes. Local film effectiveness measurements were made using a computerized pressure sensitive paint (PSP) technique. Nitrogen gas was used to simulate cooling flow as well as a tracer gas to indicate oxygen concentration such that film effectiveness by the mass transfer analogy. Three separate nozzle test models were fabricated, which have same cooling supply plenum configurations. One of them has a row of shaped hole on the pressure surface without a compound angle. The other two test models have same size film holes at the same location, but one with a 30-degree compound angle in co-flow and the other in counter-flow direction to the cooling supply. Four cooling mass flow ratios (MFR, blowing ratio) were studied for each of the nozzle test models and two-dimensional film effectiveness distributions were measured. Then the film effectiveness distributions were spanwise averaged for comparison. For all three cases, the overall film effectiveness increased with the MFR (or the blowing ratio), but not significantly. Film effectiveness by a compound angle injection is higher compared to those without a compound angle near the injection, further downstream the difference is insignificant.
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9

Iki, Norihiko, Takahiro Inoue, Takayuki Matsunuma, Hiro Yoshida, Satoshi Sodeoka, Masato Suzuki, Takumi Ebara, and Yoonhwan Lee. "Micro Gas Turbine With Ceramic Nozzles and Rotor: Part 2." In ASME Turbo Expo 2006: Power for Land, Sea, and Air. ASMEDC, 2006. http://dx.doi.org/10.1115/gt2006-90328.

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In order to develop a micro gas turbine with high turbine inlet temperature and thermal efficiency, a series of running tests has been carried out. J-850 jet engine (Sophia Precision Co., Ltd.) was chosen as a baseline machine. The turbine nozzle and the rotor are replaced by type SN-01 (Otsuka Ceramics Co., Ltd.) and type SN-235 (Kyocera Corporation) ceramic elements, respectively. By using type 3a engine, we succeeded one-hour running test of the engine without cooling and severe damages. The turbine inlet temperature was higher than 1000 °C. The rotating speed was about 120,000 rpm. Performances of the type 3a engine (with ceramic nozzle and rotor) and the type 1 (with Inconel alloy nozzle and ceramic rotor) were compared as follows: At the same rotation speed, turbine inlet temperature of the type 3a became higher than that of the type 1. Simultaneously, fuel consumption of type 3a was larger than that of the type 1. Thrust of the type 3a was slightly larger than that of the type 1. Those results imply that the thermal efficiency of type 3a is slightly, 2%, lower than that of the type 1. The present sealing configurations between ceramic nozzle-vanes and their holder plate and ceramic rotor-housing and metal combustion chamber were found to work well.
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10

Iki, Norihiko, Takahiro Inoue, Takayuki Matsunuma, Hiro Yoshida, Satoshi Sodeoka, and Masato Suzuki. "Gas Turbine With Ceramic and Metal Components." In ASME Turbo Expo 2007: Power for Land, Sea, and Air. ASMEDC, 2007. http://dx.doi.org/10.1115/gt2007-27630.

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To obtain a micro gas turbine with high turbine inlet temperature and efficiency, a series of running tests has been carried out. J-850 jet engine (Sophia Precision Co., Ltd.) was chosen as a base line machine. The turbine nozzle and the rotor are replaced to ceramic type. The observed problems occurring during the running test taught us various measures to improve heat tolerance of the engine. Especially, the ceramic nozzle vanes can be installed on a metal disk very simply. The disk structure enables us to replace blades with various shape and attack angles. We tried to operate several sets of ceramic components and metal components, such as a set of a ceramic turbine nozzle and an Inconel rotor, etc.
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